DISTRIBUTION MODULE FOR A PROPULSION MODULE OF A PROJECTILE LAUNCHER

Description

FIELD OF THE INVENTION

Embodiments of the present disclosure relate to a projectile launcher.

BRIEF DESCRIPTION OF THE DRAWINGS

The subject matter of the present disclosure is particularly pointed out and distinctly claimed in the concluding portion of the specification. A more complete understanding of the present disclosure, however, may best be obtained by referring to the detailed description and claims when considered in connection with the following illustrative figures. In the following figures, like reference numbers refer to similar elements and steps throughout the figures.

FIG. 1A is a perspective view of a projectile launcher, in accordance with various embodiments;

FIG. 1B is a perspective view of a handle and a magazine for the projectile launcher of FIG. 1A, in accordance with various embodiments;

FIG. 1C is a schematic view of the projectile launcher of FIG. 1A, in accordance with various embodiments;

FIG. 2A is a front perspective view of a magazine for a projectile launcher, in accordance with various embodiments;

FIG. 2B is a rear perspective view of a magazine for a projectile launcher, in accordance with various embodiments;

FIG. 3 is a block diagram illustrating a propulsion module for a projectile launcher, in accordance with various embodiments;

FIG. 4A is a front perspective view of a distribution module for a propulsion module of a projectile launcher, in accordance with various embodiments;

FIG. 4B is a rear perspective view of a distribution module for a propulsion module of a projectile launcher, in accordance with various embodiments;

FIG. 4C is an exploded front perspective view of a distribution module for a propulsion module of a projectile launcher, in accordance with various embodiments;

FIG. 4D is an exploded rear perspective view of a distribution module for a propulsion module of a projectile launcher, in accordance with various embodiments;

FIG. 5A is a front perspective view of a distribution module in a first position, in accordance with various embodiments;

FIG. 5B is a cross-sectional view of a distribution module in a first position, in accordance with various embodiments;

FIG. 6A is a front perspective view of a distribution module in a second position, in accordance with various embodiments;

FIG. 6B is a cross-sectional view of a distribution module in a second position, in accordance with various embodiments;

FIG. 7A is a first side perspective view of a trigger control assembly interfacing with a distribution module, in accordance with various embodiments;

FIG. 7B is a second side perspective view of a trigger control assembly interfacing with a distribution module, in accordance with various embodiments;

FIG. 8A is a side perspective view of a trigger control assembly in a first position while interfacing with a distribution module, in accordance with various embodiments;

FIG. 8B is a side perspective view of a trigger control assembly in a second position while interfacing with a distribution module, in accordance with various embodiments;

FIG. 8C is a side perspective view of a trigger control assembly in a third position while interfacing with a distribution module, in accordance with various embodiments;

FIG. 9A is a partial schematic view of a projectile launcher with a translating distribution module, in accordance with various embodiments;

FIG. 9B is a first perspective view of the projectile launcher of FIG. 9A, in accordance with various embodiments;

FIG. 9C is a second perspective view of the projectile launcher of FIG. 9A, in accordance with various embodiments;

FIG. 10A is a schematic view including a cross-sectional view of a distribution module in a resting position, in accordance with various embodiments;

FIG. 10B is a schematic view including a cross-sectional view of a distribution module in a deployment position, in accordance with various embodiments; and

FIG. 11 is a process flow for a method of deploying a projectile using a distribution module of a propulsion module, in accordance with various embodiments.

Elements and steps in the figures are illustrated for simplicity and clarity and have not necessarily been rendered according to any particular sequence. For example, steps that may be performed concurrently or in different order are illustrated in the figures to help to improve understanding of embodiments of the present disclosure.

DETAILED DESCRIPTION

The detailed description of exemplary embodiments herein makes reference to the accompanying drawings, which show exemplary embodiments by way of illustration. While these embodiments are described in sufficient detail to enable those skilled in the art to practice the disclosures, it should be understood that other embodiments may be realized and that logical changes and adaptations in design and construction may be made in accordance with this disclosure and the teachings herein. Thus, the detailed description herein is presented for purposes of illustration only and not of limitation.

The scope of the disclosure is defined by the appended claims and their legal equivalents rather than by merely the examples described. For example, the steps recited in any of the method or process descriptions may be executed in any order and are not necessarily limited to the order presented. Furthermore, any reference to singular includes plural embodiments, and any reference to more than one component or step may include a singular embodiment or step. Reference to attached, fixed, coupled, connected, or the like may include permanent, removable, temporary, partial, full, and/or any other possible attachment option. Surface shading lines may be used throughout the figures to denote different parts but not necessarily to denote the same or different materials.

In various embodiments, a projectile launcher may be configured to launch one or more projectiles towards a target. A projectile launcher may comprise any platform, device, weapon, gun, system, and/or the like configured to deploy (or cause deployment of) a projectile. For example, a projectile launcher may comprise one or more electronic devices configured to deploy a projectile. As a further example, a projectile launcher may comprise a conducted electrical weapon (CEW), a modular conducted electrical weapon (MCEW), a payload launcher, a projectile device configured to deploy entangling projectiles, a paintball gun, and/or the like. In that regard, the projectile launcher may comprise a standalone device, a device mounted or in communication with a second device, a platform, device, or system in electronic communication with a second electronic device, and/or the like.

In various embodiments, a projectile launcher may be configured to be held and operated by a human user. For example, the projectile launcher may comprise a handle, a grip, a barrel, a stock, and/or the like configured to be held in a hand of the human user.

In various embodiments, a projectile launcher may be mounted on or proximate to a platform. In that regard, the projectile launcher may be remotely operated. For example, a human user may remotely operate the projectile launcher. The platform may comprise any suitable object, structure, or the like.

For example, in some embodiments the platform may comprise a remote vehicle. The remote vehicle may comprise any object capable of traveling by land (e.g., surfaces), water, or air. The remote vehicle may be operated by a human user. The remote vehicle may comprise an autonomous vehicle. The remote vehicle may comprise an unmanned aerial vehicle (UAV) (e.g., a drone), an unmanned ground vehicle (UGV), an unmanned surface vessel (USV) (e.g., unmanned surface vehicle, autonomous surface vehicle, etc.), a robot, a car, or the like. A ground vehicle may comprise one or more wheels, a continuous track (e.g., tank tread, caterpillar track, etc.), or the like configured to enable movement of the vehicle on land-based terrain. The remote vehicle may be operable via a separate control interface. The remote vehicle may be operable via a short-range electronic communication and/or via a long-range electronic communication. In various embodiments, the decision to remotely deploy a projectile launcher from a platform may be received directly from a human operator.

As a further example, in some embodiments the platform may comprise a static structure. The static structure may comprise a security pole, a building wall (internal or external), a wall or surface of an access control vestibule (e.g., an air lock, a mantrap, a sally port, etc.), a surface of a vehicle, a surface or exterior surface of an electronic device (e.g., a recording device, a CCTV camera, etc.), and/or the like.

A projectile launcher may be configured to launch any suitable type of projectile. For example, a projectile may include any object, payload, capsule, and/or the like configured to be deployed from a projectile launcher. For example, and in accordance with various embodiments, a projectile may comprise a non-lethal or less-lethal projectile. In that regard a projectile may comprise or be configured to deploy a dart, a paintball, a rubber projectile (e.g., a rubber bullet), a conducted electrical weapon (CEW) electrode, a modular conducted electrical weapon (MCEW) electrode or payload, an entangling projectile configured to entangle a target (e.g., a tether-based entangling projectile, a net, etc.), a scent-based projectile, a liquid-based projectile, a gas-based projectile, pepper spray or a pepper spray projectile (e.g., oleoresin capsicum, OC spray), tear gas or a tear gas cannister or projectile (e.g., 2-chlorobenzalmalononitrile, CS spray), and/or any other non-lethal or less-lethal projectile.

In various embodiments, an electrode for a CEW include a spear portion, designed to pierce or attach proximate a tissue of a target in order to provide a conductive electrical path between the electrode and the tissue. For example, the electrode may be electrically coupled to a handle of the projectile launcher via a conductive filament wire. The handle may provide an electrical current through the filament wire, the electrode, the spear, and to the target.

In some embodiments, a projectile may be configured to deliver an inhibitory substance (e.g., to at least partially inhibit a target). In some embodiments, a projectile may be configured to deliver a marking substance (e.g., to mark or designate a target).

In various embodiments, a projectile launcher may be used to interfere with voluntary locomotion (e.g., walking, running, moving, etc.) of a target. For example, a projectile launcher may comprise a CEW. A CEW may be used to deliver a current (e.g., stimulus signal, pulses of current, pulses of charge, etc.) through tissue of a human or animal target. Although typically referred to as a conducted electrical weapon, as described herein a “CEW” may refer to a conducted electrical weapon, a conducted energy weapon (or “energy weapon”), an electronic control device, an electroshock weapon, and/or any other similar device or apparatus configured to provide a stimulus signal through one or more deployed projectiles (e.g., electrodes).

A CEW may be configured to deliver a stimulus signal to a target. The stimulus signal carries a charge into target tissue. The stimulus signal may interfere with voluntary locomotion of the target. The stimulus signal may cause pain. The pain may also function to encourage the target to stop moving. The stimulus signal may cause skeletal muscles of the target to become stiff (e.g., lock up, freeze, etc.). The stiffening of the muscles in response to a stimulus signal may be referred to as neuromuscular incapacitation (“NMI”). NMI disrupts voluntary control of the muscles of the target. The inability of the target to control its muscles interferes with locomotion of the target.

A stimulus signal may be delivered through the target via terminals coupled to the CEW. Delivery via terminals may be referred to as a local delivery (e.g., a local stun, a drive stun, etc.). During local delivery, the terminals are brought close to the target by positioning the CEW proximate to the target. The stimulus signal is delivered through the target's tissue via the terminals. To provide local delivery, the user of the CEW is generally within arm's reach of the target and brings the terminals of the CEW into contact with or proximate to the target.

A stimulus signal may be delivered through the target via one or more (typically at least two) wire-tethered electrodes. Delivery via wire-tethered electrodes may be referred to as a remote delivery (e.g., a remote stun). During a remote delivery, the CEW may be separated from the target up to the length (e.g., 15 feet, 20 feet, 30 feet, etc.) of the wire tether. The CEW launches the electrodes towards the target. As the electrodes travel toward the target, the respective wire tethers deploy behind the electrodes. The wire tether electrically couples the CEW to the electrode. The electrode may electrically couple to the target thereby coupling the CEW to the target. In response to the electrodes connecting with, impacting on, or being positioned proximate to the target's tissue, the current may be provided through the target via the electrodes (e.g., a circuit is formed through the first tether and the first electrode, the target's tissue, and the second electrode and the second tether).

Terminals or electrodes that contact or are proximate to the target's tissue deliver the stimulus signal through the target. Contact of a terminal or electrode with the target's tissue establishes an electrical coupling (e.g., circuit) with the target's tissue. Electrodes may include a spear that may pierce the target's tissue to contact the target. A terminal or electrode that is proximate to the target's tissue may use ionization to establish an electrical coupling with the target's tissue. Ionization may also be referred to as arcing.

In use (e.g., during deployment), a terminal or electrode may be separated from the target's tissue by the target's clothing or a gap of air. In various embodiments, a signal generator of the CEW may provide the stimulus signal (e.g., current, pulses of current, etc.) at a high voltage (e.g., in the range of 40,000 to 100,000 volts) to ionize the air in the clothing or the air in the gap that separates the terminal or electrode from the target's tissue. Ionizing the air establishes a low impedance ionization path from the terminal or electrode to the target's tissue that may be used to deliver the stimulus signal into the target's tissue via the ionization path. The ionization path persists (e.g., remains in existence, lasts, etc.) as long as the current of a pulse of the stimulus signal is provided via the ionization path. When the current ceases or is reduced below a threshold (e.g., amperage, voltage), the ionization path collapses (e.g., ceases to exist) and the terminal or electrode is no longer electrically coupled to the target's tissue. Lacking the ionization path, the impedance between the terminal or electrode and target tissue is high. A high voltage in the range of about 50,000 volts can ionize air in a gap of up to about one inch.

A CEW may provide a stimulus signal as a series of current pulses. Each current pulse may include a high voltage portion (e.g., 40,000-100,000 volts) and a low voltage portion (e.g., 500-6,000 volts). The high voltage portion of a pulse of a stimulus signal may ionize air in a gap between an electrode or terminal and a target to electrically couple the electrode or terminal to the target. In response to the electrode or terminal being electrically coupled to the target, the low voltage portion of the pulse delivers an amount of charge into the target's tissue via the ionization path. In response to the electrode or terminal being electrically coupled to the target by contact (e.g., touching, spear embedded into tissue, etc.), the high portion of the pulse and the low portion of the pulse both deliver charge to the target's tissue. Generally, the low voltage portion of the pulse delivers a majority of the charge of the pulse into the target's tissue. In various embodiments, the high voltage portion of a pulse of the stimulus signal may be referred to as the spark or ionization portion. The low voltage portion of a pulse may be referred to as the muscle portion.

In various embodiments, a signal generator of the CEW may provide the stimulus signal (e.g., current, pulses of current, etc.) at a low voltage (e.g., less than 2,000 volts). The low voltage stimulus signal may not ionize the air in the clothing or the air in the gap that separates the terminal or electrode from the target's tissue. A CEW having a signal generator providing stimulus signals at only a low voltage (e.g., a low voltage signal generator) may require deployed electrodes to be electrically coupled to the target by contact (e.g., touching, spear embedded into tissue, etc.).

In some embodiments, a CEW may include at least two terminals at the face of the CEW. A CEW may include two terminals for each bay that accepts a magazine (e.g., deployment unit). The terminals are spaced apart from each other. In response to the electrodes of the magazine in the bay having not been deployed, the high voltage impressed across the terminals will result in ionization of the air between the terminals. The arc between the terminals may be visible to the naked eye. In response to a launched electrode not electrically coupling to a target, the current that would have been provided via the electrodes may arc across the face of the CEW via the terminals.

The likelihood that the stimulus signal will cause NMI increases when the electrodes that deliver the stimulus signal are spaced apart at least 6 inches (15.24 centimeters) so that the current from the stimulus signal flows through the at least 6 inches of the target's tissue. In various embodiments, the electrodes preferably should be spaced apart at least 12 inches (30.48 centimeters) on the target. Because the terminals on a CEW are typically less than 6 inches apart, a stimulus signal delivered through the target's tissue via terminals likely will not cause NMI, only pain.

A series of pulses may include two or more pulses separated in time. Each pulse delivers an amount of charge into the target's tissue. In response to the electrodes being appropriately spaced (as discussed above), the likelihood of inducing NMI increases as each pulse delivers an amount of charge in the range of 55 microcoulombs to 71 microcoulombs per pulse. The likelihood of inducing NMI increases when the rate of pulse delivery (e.g., rate, pulse rate, repetition rate, etc.) is between 11 pulses per second (“pps”) and 50 pps. Pulses delivered at a higher rate may provide less charge per pulse to induce NMI. Pulses that deliver more charge per pulse may be delivered at a lesser rate to induce NMI. In various embodiments, a CEW may be hand-held and use batteries to provide the pulses of the stimulus signal. In response to the amount of charge per pulse being high and the pulse rate being high, the CEW may use more energy than is needed to induce NMI. Using more energy than is needed depletes batteries more quickly.

Empirical testing has shown that the power of the battery may be conserved with a high likelihood of causing NMI in response to the pulse rate being less than 44 pps and the charge per a pulse being about 63 microcoulombs. Empirical testing has shown that a pulse rate of 22 pps and 63 microcoulombs per a pulse via a pair of electrodes will induce NMI when the electrode spacing is at least 12 inches (30.48 centimeters).

In various embodiments, a projectile launcher may include a handle and one or more magazines (e.g., deployment units, etc.). The handle may include one or more bays for receiving the magazine(s). The magazine(s) may be removably positioned in (e.g., inserted into, coupled to, etc.) a bay. The magazine(s) may releasably electrically, electronically, and/or mechanically couple to a bay. A deployment of the projectile launcher may launch one or more projectiles from the magazine. For example, a deployment of the projectile launcher may cause one or more projectiles to be launched toward a target. In embodiments where the projectile launcher comprises a CEW, deployment of the projectile launcher may cause one or more projectiles to be launched toward a target to remotely deliver a stimulus signal through the target.

In various embodiments, a magazine may be configured to include, hold, or receive one or more projectiles. A magazine may include two or more projectiles that are launched at a same time. A magazine may include two or more projectiles that may each be launched individually at separate times. A magazine may include a single projectile configured to be launched from the magazine. Launching the projectiles may be referred to as activating (e.g., firing, deploying, launching, etc.) a magazine or projectile launcher. After use (e.g., after activation), a magazine may be removed from the bay and reloaded with new projectiles and/or replaced with an unused (e.g., not fired, not activated) magazine to permit launch of additional projectile(s).

In various embodiments, and with reference to FIGS. 1A-1C, a projectile launcher 100 is disclosed. Projectile launcher 100 may be similar to, or have similar aspects and/or components with, any projectile launcher, CEW, or the like discussed herein. Projectile launcher 100 may comprise a handle 110 and a magazine 112. It should be understood by one skilled in the art that FIG. 1C is a schematic representation of projectile launcher 100, and one or more of the components of projectile launcher 100 may be located in any suitable position within, or external to, handle 110.

Handle 110 may be configured to house various components of projectile launcher 100 that are configured to enable deployment of projectiles from magazine 112, provide an electrical current to magazine 112, and otherwise aid in the operation of projectile launcher 100, as discussed further herein. Although depicted with firearm shape in FIGS. 1A and 1B, handle 110 may comprise any suitable shape and/or size. Handle 110 may comprise a handle end 113 opposite a deployment end 114. Deployment end 114 may be configured, and sized and shaped, to receive one or more magazine 112. Handle end 113 may be sized and shaped to be held in a hand of a user. For example, handle end 113 may be shaped as a handle to enable hand-operation of projectile launcher 100 by the user. In various embodiments, handle end 113 may also comprise contours shaped to fit the hand of a user, for example, an ergonomic grip. Handle end 113 may include a surface coating, such as, for example, a non-slip surface, a grip pad, a rubber texture, and/or the like. As a further example, handle end 113 may be wrapped in leather, a colored print, and/or any other suitable material, as desired.

In various embodiments, handle 110 may comprise various mechanical, electronic, and/or electrical components configured to aid in performing the functions of projectile launcher 100. For example, handle 110 may comprise one or more triggers 115, control interfaces 117, processing circuits 135, power supplies 140, and/or signal generators 145. Handle 110 may include a guard (e.g., trigger guard). A guard may define an opening formed in handle 110. A guard may be located on a center region of handle 110 (e.g., as depicted in FIGS. 1A and 1B), and/or in any other suitable location on handle 110. Trigger 115 may be disposed within a guard. A guard may be configured to protect trigger 115 from unintentional physical contact (e.g., an unintentional activation of trigger 115). A guard may surround trigger 115 within handle 110.

In various embodiments, trigger 115 be coupled to an outer surface of handle 110, and may be configured to move, slide, rotate, or otherwise become physically depressed or moved upon application of physical contact. For example, trigger 115 may be actuated by physical contact applied to trigger 115 from within a guard. Trigger 115 may comprise a mechanical or electromechanical switch, button, trigger, or the like. For example, trigger 115 may comprise a switch, a pushbutton, and/or any other suitable type of trigger. Trigger 115 may be mechanically and/or electronically coupled to processing circuit 135. In response to trigger 115 being activated (e.g., depressed, pushed, etc. by the user), processing circuit 135 may enable deployment of (or cause deployment of) one or more magazine 112 from projectile launcher 100, as discussed further herein.

In various embodiments, power supply 140 may be configured to provide power to various components of projectile launcher 100. For example, power supply 140 may provide energy for operating the electronic and/or electrical components (e.g., parts, subsystems, circuits, etc.) of projectile launcher 100 and/or one or more magazine 112. Power supply 140 may provide electrical power. Providing electrical power may include providing a current at a voltage. Power supply 140 may be electrically coupled to processing circuit 135 and/or signal generator 145. In various embodiments, in response to a control interface comprising electronic properties and/or components, power supply 140 may be electrically coupled to the control interface. In various embodiments, in response to trigger 115 comprising electronic properties or components, power supply 140 may be electrically coupled to trigger 115. Power supply 140 may provide an electrical current at a voltage. Electrical power from power supply 140 may be provided as a direct current (“DC”). Electrical power from power supply 140 may be provided as an alternating current (“AC”). Power supply 140 may include a battery. The energy of power supply 140 may be renewable or exhaustible, and/or replaceable. For example, power supply 140 may comprise one or more rechargeable or disposable batteries. In various embodiments, the energy from power supply 140 may be converted from one form (e.g., electrical, magnetic, thermal) to another form to perform the functions of a system.

Power supply 140 may provide energy for performing the functions of projectile launcher 100. For example, power supply 140 may provide the electrical current to signal generator 145 that is provided through a target to impede locomotion of the target (e.g., via magazine 112). Power supply 140 may provide the energy for a stimulus signal. Power supply 140 may provide the energy for other signals, including an ignition signal, as discussed further herein.

In various embodiments, processing circuit 135 may comprise any circuitry, electrical components, electronic components, software, and/or the like configured to perform various operations and functions discussed herein. For example, processing circuit 135 may comprise a processing circuit, a processor, a digital signal processor, a microcontroller, a microprocessor, an application specific integrated circuit (ASIC), a programmable logic device, logic circuitry, state machines, microelectromechanical systems (MEMS) devices, signal conditioning circuitry, communication circuitry, a computer, a computer-based system, a radio, a network appliance, a data bus, an address bus, and/or any combination thereof. In various embodiments, processing circuit 135 may include passive electronic devices (e.g., resistors, capacitors, inductors, etc.) and/or active electronic devices (e.g., op amps, comparators, analog-to-digital converters, digital-to-analog converters, programmable logic, status relay controls (SRCs), transistors, etc.). In various embodiments, processing circuit 135 may include data buses, output ports, input ports, timers, memory, arithmetic units, and/or the like.

In various embodiments, processing circuit 135 may include signal conditioning circuity. Signal conditioning circuitry may include level shifters to change (e.g., increase, decrease) the magnitude of a voltage (e.g., of a signal) before receipt by processing circuit 135 or to shift the magnitude of a voltage provided by processing circuit 135.

In various embodiments, processing circuit 135 may be configured to control and/or coordinate operation of some or all aspects of projectile launcher 100. For example, processing circuit 135 may include (or be in communication with) memory configured to store data, programs, and/or instructions. The memory may comprise a tangible non-transitory computer-readable memory. Instructions stored on the tangible non-transitory memory may allow processing circuit 135 to perform various operations, functions, and/or steps, as described herein.

The term “non-transitory” as used herein is to be understood to remove only propagating transitory signals per se from the claim scope and does not relinquish rights to all standard computer-readable media that are not only propagating transitory signals per se. Stated another way, the meaning of the term “non-transitory computer-readable memory,” “non-transitory memory,” and similar phrases should be construed to exclude only those types of transitory computer-readable media which were found in In re Nuijten to fall outside the scope of patentable subject matter under 35 U.S.C. § 101.

In various embodiments, the memory may comprise any hardware, software, and/or database component capable of storing and maintaining data. For example, a memory unit may comprise a database, data structure, memory component, or the like. A memory unit may comprise any suitable non-transitory memory known in the art, such as, an internal memory (e.g., random access memory (RAM), read-only memory (ROM), solid state drive (SSD), etc.), removable memory (e.g., an SD card, an xD card, a CompactFlash card, etc.), or the like.

Processing circuit 135 may be configured to provide and/or receive electrical signals whether digital and/or analog in form. Processing circuit 135 may provide and/or receive digital information via a data bus using any protocol. Processing circuit 135 may receive information, manipulate the received information, and provide the manipulated information. Processing circuit 135 may store information and retrieve stored information. Information received, stored, and/or manipulated by processing circuit 135 may be used to perform a function, control a function, and/or to perform an operation or execute a stored program.

Processing circuit 135 may control the operation and/or function of other circuits and/or components of projectile launcher 100. Processing circuit 135 may receive or determine status information regarding the operation of other components, perform calculations with respect to the status information, and provide commands (e.g., instructions) to one or more other components. Processing circuit 135 may command another component to start operation, continue operation, alter operation, suspend operation, cease operation, or the like. Commands and/or status may be communicated between processing circuit 135 and other circuits and/or components via any suitable electrical signal or electronic communication. Commands and/or status may be communicated between processing circuit 135 and other circuits and/or components via any type of bus (e.g., SPI bus) including any type of data/address bus.

In various embodiments, processing circuit 135 may comprise or be in electronic communication with a communications unit. The communications unit may be similar to, or comprise similar components with, any other communications unit, short-range communications unit, long-range communications unit, or the like disclosed here. The communications unit may enable electronic communications between devices and systems. The communications unit may enable communications over a network. For example, the communications unit may include a modem, a network interface (such as an Ethernet card), a communications port, or the like. Data may be transferred via the communications unit in the form of signals which may be electronic, electromagnetic, optical, or other signals capable of being transmitted or received by a communications unit. The communications unit may be configured to communicate via any wired protocol, wireless protocol, or other protocol capable of transmitting information via a wired or wireless connection. In various embodiments, the communications unit may be configured to enable short-range communications between devices. In various embodiments, the communications unit may be configured to enable long-range communications between devices or systems. In various embodiments, the communications unit may be configured to enable both short-range communications and long-range communications.

In various embodiments, processing circuit 135 may be mechanically and/or electronically coupled to trigger 115. In various embodiments, processing circuit 135 may be electrically coupled to a switch or other electrical component associated with or activated by trigger 115. Processing circuit 135 may be configured to detect an activation, actuation, depression, input, etc. (collectively, an “activation event”) of trigger 115. In response to detecting the activation event, processing circuit 135 may be configured to perform various operations and/or functions, as discussed further herein. Processing circuit 135 may also include a sensor (e.g., a trigger sensor) attached to or activated by trigger 115 and configured to detect or receive activation of an activation event of trigger 115. The sensor may comprise any suitable sensor, such as a mechanical and/or electronic sensor capable of detecting or receiving an activation event in trigger 115 and reporting the activation event to processing circuit 135.

In various embodiments, processing circuit 135 may be mechanically and/or electronically coupled to control interface 117. In various embodiments, processing circuit 135 may be electrically coupled to a switch or other electrical component associated with or activated by control interface 117. Processing circuit 135 may be configured to detect or receive an activation, actuation, depression, input, signal, communication, etc. (collectively, a “control event”) of control interface 117. In response to detecting or receiving the control event, processing circuit 135 may be configured to perform various operations and/or functions, as discussed further herein. Processing circuit 135 may also include a sensor (e.g., a control sensor) attached to or activated by control interface 117 and configured to detect or receive activation of a control event of control interface 117. The sensor may comprise any suitable sensor, such as a mechanical and/or electronic sensor capable of detecting or receiving a control event in control interface 117 and reporting the control event to processing circuit 135.

In various embodiments, processing circuit 135 may be electrically and/or electronically coupled to power supply 140. Processing circuit 135 may receive power from power supply 140. The power received from power supply 140 may be used by processing circuit 135 to receive signals, process signals, and transmit signals to various other components in projectile launcher 100. Processing circuit 135 may use power from power supply 140 to detect or receive an activation event of trigger 115, a control event of control interface 117, or the like, and generate one or more control signals in response to the detected events. The control signal may be based on the control event and the activation event. The control signal may be an electrical signal.

Processing circuit 135 may control provision of power from power supply 140 to one or more other components of projectile launcher 100. For example, power may be provided to one or more other components via an electrical circuit of projectile launcher 100. The electrical circuit may comprise any suitable type of electrical circuit and may include one or more passive components and/or active components. In some embodiments, the electrical circuit may comprise one or more electrical switches configured to control provision of power to components of projectile launcher 100. Processing circuit 135 may be electrically coupled to the one or more electrical switches. Processing circuit 135 may be configured to control the electrical switches via electrical signals to close or open the electrical switches.

In various embodiments, processing circuit 135 may be electrically and/or electronically coupled to signal generator 145. Processing circuit 135 may be configured to transmit or provide control signals to signal generator 145 in response to detecting an activation event of trigger 115. Multiple control signals may be provided from processing circuit 135 to signal generator 145 in series. In response to receiving the control signal, signal generator 145 may be configured to perform various functions and/or operations, as discussed further herein. In some embodiments, control signals from processing circuit 135 to signal generator 145 may include signals from processing circuit 135 to provide power to or remove power from signal generator 145 (e.g., electrical signals to control electrical switches between power supply 140 and signal generator 145).

In various embodiments, signal generator 145 may be configured to receive one or more control signals from processing circuit 135. Signal generator 145 may provide an ignition signal to magazine 112 based on the control signals. Signal generator 145 may be electrically and/or electronically coupled to processing circuit 135 and/or magazine 112. Signal generator 145 may be electrically coupled to power supply 140. Signal generator 145 may use power received from power supply 140 to generate an ignition signal. For example, signal generator 145 may receive an electrical signal from power supply 140 that has first current and voltage values. Signal generator 145 may transform the electrical signal into an ignition signal having second current and voltage values. The transformed second current and/or the transformed second voltage values may be different from the first current and/or voltage values. The transformed second current and/or the transformed second voltage values may be the same as the first current and/or voltage values. Signal generator 145 may temporarily store power from power supply 140 and rely on the stored power entirely or in part to provide the ignition signal. Signal generator 145 may also rely on received power from power supply 140 entirely or in part to provide the ignition signal, without needing to temporarily store power.

Signal generator 145 may be controlled entirely or in part by processing circuit 135. In various embodiments, signal generator 145 and processing circuit 135 may be separate components (e.g., physically distinct and/or logically discrete). Signal generator 145 and processing circuit 135 may be a single component. For example, a control circuit within handle 110 may at least include signal generator 145 and processing circuit 135. The control circuit may also include other components and/or arrangements, including those that further integrate corresponding function of these elements into a single component or circuit, as well as those that further separate certain functions into separate components or circuits.

Signal generator 145 may be controlled by the control signals to generate an ignition signal having a predetermined current value or values. For example, signal generator 145 may include a current source. The control signal may be received by signal generator 145 to activate the current source at a current value of the current source. An additional control signal may be received to decrease a current of the current source. For example, signal generator 145 may include a pulse width modification circuit coupled between a current source and an output of the control circuit. A second control signal may be received by signal generator 145 to activate the pulse width modification circuit, thereby decreasing a non-zero period of a signal generated by the current source and an overall current of an ignition signal subsequently output by the control circuit. The pulse width modification circuit may be separate from a circuit of the current source or, alternatively, integrated within a circuit of the current source. Various other forms of signal generators 45 may alternatively or additionally be employed, including those that apply a voltage over one or more different resistances to generate signals with different currents. In various embodiments, signal generator 145 may include a high-voltage module configured to deliver an electrical current having a high voltage. In various embodiments, signal generator 145 may include a low-voltage module configured to deliver an electrical current having a lower voltage, such as, for example, 2,000 volts.

Responsive to receipt of a signal indicating activation of trigger 115 (e.g., an activation event), a control circuit provides an ignition signal to magazine 112 (or one or more projectiles P in magazine 112). For example, signal generator 145 may provide an electrical signal as an ignition signal to magazine 112 in response to receiving a control signal from processing circuit 135. In various embodiments, the ignition signal may be separate and distinct from a stimulus signal. For example, a stimulus signal in projectile launcher 100 may be provided to a different circuit within magazine 112, relative to a circuit to which an ignition signal is provided. Signal generator 145 may be configured to generate a stimulus signal. In various embodiments, a second, separate signal generator, component, or circuit (not shown) within handle 110 may be configured to generate the stimulus signal. Signal generator 145 may also provide a ground signal path for magazine 112, thereby completing a circuit for an electrical signal provided to magazine 112 by signal generator 145. The ground signal path may also be provided to magazine 112 by other elements in handle 110, including power supply 140.

In various embodiments, a bay 111 of handle 110 may be configured to receive one or more magazine 112. Bay 111 may comprise an opening in deployment end 114 sized and shaped to receive one or more magazine 112. Bay 111 may include one or more mechanical features configured to removably couple one or more magazine 112 within bay 111. Bay 111 may be configured to receive a single magazine, two magazines, three magazines, nine magazines, or any other number of magazines.

In various embodiments, magazine 112 may comprise a housing sized and shaped to be inserted into bay 111. The housing may define one or more bores. Each bore may define an opening through the housing (e.g., a chamber). Each bore may be configured to receive a projectile. Each bore may be sized and shaped accordingly to receive and house a projectile prior to and during deployment of the projectile from magazine 112. Each bore may comprise any suitable deployment angle. One or more bores may comprise similar deployment angles. One or more bores may comprise different deployment angles. The housing may comprise any suitable or desired number of bores, such as, for example, two bores, five bores, eight bores (e.g., as depicted), ten bores, and/or the like.

In various embodiments, magazine 112 may be configured to receive one or more projectiles P, such as, for example, a first projectile P0, a second projectile P1, a third projectile P2, an “Nth” projectile Pn, and/or the like. Magazine 112 may be configured to receive a number of projectile P equal to or less than a number of bores in magazine 112. Each projectile P may comprise a body and one or more components necessary to store and/or deploy the projectile P from the body. Each projectile P may be similar to any other electrode, projectile, or the like disclosed herein. As referred to herein, projectiles P0, P1, P2, Pn may be generally referred to individually as a “projectile P” or in a plurality as “projectiles P.”

In various embodiments, handle 110 may comprise a propulsion module 125. Propulsion module 125 may be configured to provide a propulsion force to deploy, or cause deployment of, one or more projectiles P. Propulsion module 125 may comprise any device, propellant, primer, or the like capable of providing a propulsion force. The propulsion force may include an increase in pressure caused by rapidly expanding gas within an arca or chamber.

Propulsion module 125 may be configured to receive a propellant from a propulsion source 130. In that regard, propulsion module 125 may be in fluid communication with propulsion source 130. Propulsion source 130 may comprise a volume of propellant configured to provide, directly or indirectly, the propulsion force. Propulsion source 130 may contain an amount of propellant under a storage pressure. The propellant may comprise any suitable propellant fluid, gas, or the like capable of deploying, or causing deployment of, a projectile P. For example, the propellant may comprise a compressed air cannister, a carbon dioxide cannister (e.g., CO2 cannister), a nitrous oxide cannister (e.g., N2O canister), a nitrogen cannister, and/or the like. In some embodiments, propulsion source 130 and/or propulsion module 125 may comprise one or more accessory systems, such as, for example, a pressure regulating system, a cannister ejection system, a pressure monitoring system, and/or the like.

Propulsion module 125 may be configured to receive an amount of propellant from propulsion source 130. For example, propulsion module 125 may receive the amount of propellant based on operation of trigger 115, control interface 117, processing circuit 135, and/or through any other suitable operation or control. As a further example, propulsion module 125 may receive the amount of propellant in response to an ignition signal, a control signal, and/or any other suitable electrical signal. The amount of propellant may comprise any volume, flow, or the like of propellant capable of deploying, or causing deployment of, one or more projectiles P.

In various embodiments, propulsion module 125 may be in electrical and/or electronic communication with processing circuit 135. In that regard, in some embodiments processing circuit 135 may control operations of propulsion module 125. For example, controlling operations may include causing propulsion module 125 to receive propellant from propulsion source 130, instructing propulsion module 125 to deliver a propulsion force to one or more projectiles P, selecting one or more projectiles P for propulsion module 125 to deliver the propulsion force to, and/or the like.

In various embodiments, propulsion module 125 may be in electrical and/or mechanical communication with trigger 115. In that regard, in some embodiments trigger 115 may control operations of propulsion module 125. For example, controlling operations may include causing propulsion module 125 to receive propellant from propulsion source 130, causing propulsion module 125 to deliver a propulsion force to one or more projectiles P, selecting one or more projectiles P for propulsion module 125 to deliver the propulsion force to, and/or the like.

In various embodiments, propulsion module 125 may be in fluid communication with magazine 112 and/or one or more projectiles P. Propulsion module 125 may be configured to provide the propulsion force to magazine 112 and/or one or more projectiles P. Receiving the propulsion force may cause one or more projectiles P to be deployed from magazine 112.

In various embodiments, the propulsion force may be directly applied to one or more projectiles P. For example, a propulsion force from propulsion module 125 may be provided directly to first projectile P1 to cause deployment of first projectile P1. Propulsion module 125 may be in fluid communication with one or more projectiles P to provide the propulsion force. For example, a propulsion force from propulsion module 125 may travel within a housing or channel of magazine 112 to first projectile P1. The propulsion force may travel via a manifold in magazine 112.

In various embodiments, the propulsion force may be provided indirectly to one or more projectiles P. For example, the propulsion force may be provided to a secondary source of propellant within propulsion module 125. The propulsion force may launch the secondary source of propellant within propulsion module 125, causing the secondary source of propellant to release propellant. A force associated with the released secondary source of propellant may in turn provide a propulsion force to one or more projectiles P. A force generated by a secondary source of propellant may cause the one or more projectiles P to be deployed from magazine 112.

In various embodiments, handle 110 and/or magazine 112 may comprise one or more interfaces. For example, handle 110 and/or magazine 112 may comprise a mechanical interface. A mechanical interface may be configured to enable magazine 112 to mechanically couple to handle 110. A mechanical interface may also be configured to at least partially seal (e.g., fluidly seal, hermetically seal, etc.) the mechanical coupling between magazine 112 and handle 110. As a further example, handle 110 and/or magazine 112 may comprise an electrical interface. An electrical interface may be configured to enable electrical signals to be provided from handle 110 to magazine 112 and/or from magazine 112 to handle 110. As a further example, handle 110 and/or magazine 112 may comprise an electronic interface. An electronic interface may be configured to enable electronic communication between handle 110 and magazine 112 (e.g., one-way communication, two-way communication, transmission of data packets, etc.). As a further example, handle 110 and/or magazine 112 may comprise a fluid interface. A fluid interface may enable handle 110 to provide a fluid (e.g., propulsion force, propellant, etc.) to magazine 112.

In various embodiments, a mechanical interface may comprise an interposer. An interposer may be configured to couple to an end of magazine 112 and at least partially seal the end of the magazine 112. The interposer may be configured to at least partially retain or couple to one or more projectiles loaded into magazine 112. The interposer may be configured to at least partially prevent electrical shorting between two or more projectiles loaded into magazine 112. The interposer may be configured to provide electrical coupling between signal generator 145 and the one or more projectiles in magazine 112 (e.g., to provide ignition signals, stimulus signals, etc.). The interposer may be configured to at least partially reduce a recoil force imparted into handle 110 in response to deployment of one or more projectiles from magazine 112. In that regard, the interposer may comprise one or more surfaces or materials configured to receive and distribute an impact load from a projectile deployment. In some embodiments, at least partially reducing the recoil force imparted from deployment of a projectile may increase the lifespan of one or more components in a projectile, magazine 112, and/or handle 110.

For example, and in accordance with various embodiments, handle 110 may comprise a first handle interface 105 and magazine 112 may comprise a first magazine interface 106. First handle interface 105 may be disposed within bay 111. First handle interface 105 may be coupled to, extend through, or be defined on an inner surface of bay 111. For example, first handle interface 105 may be coupled to, extend through, or be defined on a rear inner surface of bay 111. First magazine interface 106 may be coupled to, extend through, or be defined on an outer surface of magazine 112. For example, first magazine interface 106 may be coupled to, extend through, or be defined on a rear outer surface of magazine 112. First handle interface 105 and first magazine interface 106 may at least partially align in response to magazine 112 coupling to handle 110.

In various embodiments, first handle interface 105 and first magazine interface 106 may each comprise any number of interfaces. For example, first handle interface 105 may comprise one or more interfaces and first magazine interface 106 may comprise one or more interfaces. In that regard, first handle interface 105 may comprise one or more of a mechanical interface, an electrical interface, an electronic interface, and/or a fluid interface. First magazine interface 106 may comprise one or more of a mechanical interface, an electrical interface, an electronic interface, and/or a fluid interface. In some embodiments, first handle interface 105 and first magazine interface 106 may each comprise a same number of interfaces. In some embodiments, first handle interface 105 and first magazine interface 106 may each comprise a different number of interfaces.

In various embodiments, first handle interface 105 and first magazine interface 106 may comprise complimentary interfaces. For example, first handle interface 105 and first magazine interface 106 may each comprise a mechanical interface. The mechanical interface of first handle interface 105 may engage with the mechanical interface of first magazine interface 106 to mechanically couple magazine 112 to handle 110. The mechanical interfaces may be complimentary. For example, the mechanical interface of first handle interface 105 may comprise a female interface and the mechanical interface of first magazine interface 106 may comprise a male interface configured to engage with the female interface.

As a further example, first handle interface 105 and first magazine interface 106 may each comprise an electrical interface. The electrical interface of first handle interface 105 may engage with the electrical interface of first magazine interface 106 to electrically couple magazine 112 to handle 110. The electrical interfaces may be complimentary. For example, the electrical interface of first handle interface 105 may comprise an electrical contact and the electrical interface of first magazine interface 106 may comprise an electrical contact. The electrical contacts may be at least partially aligned and in contact to electrically couple magazine 112 to handle 110.

As a further example, first handle interface 105 and first magazine interface 106 may each comprise an electronic interface. The electronic interface of first handle interface 105 may engage with the electronic interface of first magazine interface 106 to electronically couple magazine 112 to handle 110. For example, the electronic interface of first handle interface 105 may comprise a communications unit and the electronic interface of first magazine interface 106 may comprise a communications unit. The communication units may communicate via a wired or wireless connection to electronically couple magazine 112 to handle 110. As a further example, the electronic interfaces may communicate via a physical connection, such as via electrical contacts, data ports, and/or the like.

As a further example, first handle interface 105 and first magazine interface 106 may each comprise a fluid interface. The fluid interface of first handle interface 105 may engage with the fluid interface of first magazine interface 106 to fluidly couple magazine 112 to handle 110. For example, the fluid interface of first handle interface 105 may comprise a distribution module (e.g., a fluid distribution module) configured to distribute a fluid (e.g., propulsion force) provided by propulsion module 125. The fluid interface of first magazine interface 106 may comprise a port or opening (e.g., a fluid channel, a bore in magazine 112, etc.) configured to enable the fluid to be distributed from the fluid interface of first handle interface 105 to one or more projectiles P of magazine 112.

In various embodiments, first handle interface 105 and first magazine interface 106 may each comprise a fluid interface. In various embodiments, first handle interface 105 and first magazine interface 106 may each comprise a mechanical interface and a fluid interface.

In various embodiments, handle 110 may comprise a second handle interface 107 and magazine 112 may comprise a second magazine interface 108. Second handle interface 107 may be disposed within bay 111. Second handle interface 107 may be coupled to, extend through, or be defined on an inner surface of bay 111. For example, second handle interface 107 may be coupled to, extend through, or be defined on a bottom inner surface of bay 111. Second magazine interface 108 may be coupled to, extend through, or be defined on an outer surface of magazine 112. For example, second magazine interface 108 may be coupled to, extend through, or be defined on a bottom outer surface of magazine 112. Second handle interface 107 and second magazine interface 108 may at least partially align in response to magazine 112 coupling to handle 110.

In various embodiments, second handle interface 107 and second magazine interface 108 may each comprise any number of interfaces. For example, second handle interface 107 may comprise one or more interfaces and second magazine interface 108 may comprise one or more interfaces. In that regard, second handle interface 107 may comprise one or more of a mechanical interface, an electrical interface, an electronic interface, and/or a fluid interface. Second magazine interface 108 may comprise one or more of a mechanical interface, an electrical interface, an electronic interface, and/or a fluid interface. In some embodiments, second handle interface 107 and second magazine interface 108 may each comprise a same number of interfaces. In some embodiments, second handle interface 107 and second magazine interface 108 may each comprise a different number of interfaces.

In various embodiments, second handle interface 107 and second magazine interface 108 may comprise complimentary interfaces. For example, second handle interface 107 and second magazine interface 108 may each comprise a mechanical interface. The mechanical interface of second handle interface 107 may engage with the mechanical interface of second magazine interface 108 to mechanically couple magazine 112 to handle 110. The mechanical interfaces may be complimentary. For example, the mechanical interface of second handle interface 107 may comprise a female interface and the mechanical interface of second magazine interface 108 may comprise a male interface configured to engage with the female interface. As a further example, the mechanical interface of second handle interface 107 may comprise a locking mechanism and the mechanical interface of second magazine interface 108 may comprise a complimentary opening configured to receive the locking mechanism. The locking mechanism may create mechanical interference to mechanical couple and position magazine 112 within bay 111 of handle 110.

As a further example, second handle interface 107 and second magazine interface 108 may each comprise an electrical interface. The electrical interface of second handle interface 107 may engage with the electrical interface of second magazine interface 108 to electrically couple magazine 112 to handle 110. The electrical interfaces may be complimentary. For example, the electrical interface of second handle interface 107 may comprise an electrical contact and the electrical interface of second magazine interface 108 may comprise an electrical contact. The electrical contacts may be at least partially aligned and in contact to electrically couple magazine 112 to handle 110.

As a further example, second handle interface 107 and second magazine interface 108 may each comprise an electronic interface. The electronic interface of second handle interface 107 may engage with the electronic interface of second magazine interface 108 to electronically couple magazine 112 to handle 110. For example, the electronic interface of second handle interface 107 may comprise a communications unit and the electronic interface of second magazine interface 108 may comprise a communications unit. The communication units may communicate via a wired or wireless connection to electronically couple magazine 112 to handle 110. As a further example, the electronic interfaces may communicate via a physical connection, such as via electrical contacts, data ports, and/or the like.

As a further example, second handle interface 107 and second magazine interface 108 may each comprise a fluid interface. The fluid interface of second handle interface 107 may engage with the fluid interface of second magazine interface 108 to fluidly couple magazine 112 to handle 110. For example, the fluid interface of second handle interface 107 may comprise a distribution module (e.g., a fluid distribution module) configured to distribute a fluid (e.g., propulsion force) provided by propulsion module 125. The fluid interface of second magazine interface 108 may comprise a port or opening (e.g., a fluid channel, a bore in magazine 112, etc.) configured to enable the fluid to be distributed from the fluid interface of second handle interface 107 to one or more projectiles P of magazine 112.

In various embodiments, second handle interface 107 and second magazine interface 108 may each comprise an electrical interface. In various embodiments, second handle interface 107 and second magazine interface 108 may each comprise a mechanical interface and an electrical interface.

In various embodiments, first handle interface 105 and first magazine interface 106 (collectively, the first interfaces) and second handle interface 107 and second magazine interface 108 (collectively, the second interfaces) may each provide at least one same or similar type of interface. For example, the first interfaces may provide at least one mechanical interface and the second interfaces may provide at least one mechanical interface. The mechanical interfaces of the first interfaces and the second interfaces may be the same or similar, or may be different. For example, the mechanical interfaces may each be mechanical alignment interfaces. As a further example, the mechanical interface of the first interfaces may comprise a mechanical scaling interface and the mechanical interface of the second interfaces may comprise a mechanical alignment interface, a mechanical locking interface, or the like.

In various embodiments, first handle interface 105 and first magazine interface 106 (collectively, the first interfaces) and second handle interface 107 and second magazine interface 108 (collectively, the second interfaces) may each provide at least one different type of interface. For example, the first interfaces may provide a fluid interface and the second interfaces may provide an electrical interface.

In various embodiments, projectile launcher 100 may deliver a stimulus signal via a circuit that includes signal generator 145 positioned in handle 110. An interface (e.g., cartridge interface, magazine interface, etc.) on each magazine 112 inserted into handle 110 electrically couples to an interface (e.g., handle interface, housing interface, etc.) in handle 110. For example, signal generator 145 may be in electrical series with second handle interface 107. Second magazine interface 108 may be electrically coupled to second handle interface 107. In that regard, signal generator 145 may be in electrical series with magazine 112 via second handle interface 107 and second magazine interface 108. Second magazine interface 108 may be in electrical series with one or more projectiles P housing in magazine 112. In that regard, a stimulus signal provided by signal generator 145 may be provided to one or more projectiles P via second handle interface 107 and second magazine interface 108. For example, a first filament wire of first projectile P1 may be electrically coupled to a first electrical interface (e.g., a positive interface) of second magazine interface 108. A second filament wire of second projectile P2 may be electrically coupled to a second electrical interface (e.g., a negative interface, a ground interface, etc.) of second magazine interface 108. The stimulus signal travels from signal generator 145, through the first electrical interface of second magazine interface 108, the first filament, first projectile P1, and tissue of a target, and returns through second projectile P2, the second filament, the second electrical interface of second magazine interface 108, and back to signal generator 145.

In various embodiments, control interface 117 may comprise, or be similar to, any control interface disclosed herein. Control interface 117 may be configured to control selection of firing modes in projectile launcher 100. Controlling selection of firing modes in projectile launcher 100 may include disabling deployment from projectile launcher 100 (e.g., a safety mode, etc.), enabling deployment from projectile launcher 100 (e.g., an active mode, a firing mode, an escalation mode, etc.), controlling deployment of magazine 112, and/or similar operations, as discussed further herein. In various embodiments, control interface 117 may also be configured to perform (or cause performance of) one or more operations that do not include the selection of firing modes. For example, control interface 117 may be configured to enable the selection of operating modes of projectile launcher 100, selection of options within an operating mode of projectile launcher 100, or similar selection or scrolling operations, as discussed further herein.

Control interface 117 may be located in any suitable location on or in handle 110. For example, control interface 117 may be coupled to an outer surface of handle 110. Control interface 117 may be coupled to an outer surface of handle 110 proximate trigger 115 and/or a guard of handle 110. Control interface 117 may be electrically, mechanically, and/or electronically coupled to processing circuit 135. In various embodiments, in response to control interface 117 comprising electronic properties or components, control interface 117 may be electrically coupled to power supply 140. Control interface 117 may receive power (e.g., electrical current) from power supply 140 to power the electronic properties or components.

Control interface 117 may be electronically or mechanically coupled to trigger 115. For example, and as discussed further herein, control interface 117 may function as a safety mechanism. In response to control interface 117 being set to a “safety mode,” projectile launcher 100 may be unable to launch projectiles P from magazine 112. For example, control interface 117 may provide a signal (e.g., a control signal) to processing circuit 135 instructing processing circuit 135 to disable deployment of projectiles P from magazine 112. As a further example, control interface 117 may electronically or mechanically prohibit trigger 115 from activating (e.g., prevent or disable a user from depressing trigger 115; prevent trigger 115 from launching a projectile P; etc.).

Control interface 117 may comprise any suitable electronic or mechanical component capable of enabling selection of firing modes. For example, control interface 117 may comprise a fire mode selector switch, a safety switch, a safety catch, a rotating switch, a selection switch, a selective firing mechanism, and/or any other suitable mechanical control. As a further example, control interface 117 may comprise a slide, such as a handgun slide, a reciprocating slide, or the like. As a further example, control interface 117 may comprise a touch screen, user interface or display, or similar electronic visual component.

The safety mode may be configured to prohibit deployment of a projectile P from magazine 112 in projectile launcher 100. For example, in response to a user selecting the safety mode, control interface 117 may transmit a safety mode instruction to processing circuit 135. In response to receiving the safety mode instruction, processing circuit 135 may prohibit deployment of a projectile P from magazine 112. Processing circuit 135 may prohibit deployment until a further instruction is received from control interface 117 (e.g., a firing mode instruction). As previously discussed, control interface 117 may also, or alternatively, interact with trigger 115 to prevent activation of trigger 115. In various embodiments, the safety mode may also be configured to prohibit provision of a stimulus signal from signal generator 145.

The firing mode may be configured to enable deployment of one or more projectiles P from magazine 112. For example, and in accordance with various embodiments, in response to a user selecting the firing mode, control interface 117 may transmit a firing mode instruction to processing circuit 135. In response to receiving (or determining) the firing mode instruction, processing circuit 135 may enable deployment of one or more projectiles P from magazine 112. In that regard, in response to trigger 115 being activated, processing circuit 135 may cause the deployment of one or more projectiles P. Processing circuit 135 may enable deployment until a further instruction is received (or determined) from control interface 117 (e.g., a safety mode instruction). As a further example, and in accordance with various embodiments, in response to a user selecting the firing mode, control interface 117 may also mechanically (or electronically) interact with trigger 115 to enable activation of trigger 115.

In various embodiments, projectile launcher 100 may further comprise one or more user interfaces. A user interface may be configured to receive an input from a user of projectile launcher 100 and/or transmit or provide an output to the user of projectile launcher 100. The user interface may be part of control interface 117. The user interface may be a distinct component of projectile launcher 100 separate from control interface 117. The user interface may be located in any suitable location on or in handle 110. For example, the user interface may be coupled to an outer surface of handle 110, or extend at least partially through the outer surface of handle 110. The user interface may be electrically, mechanically, and/or electronically coupled to processing circuit 135. In various embodiments, in response to the user interface comprising electronic or electrical properties or components, the user interface may be electrically coupled to power supply 140. The user interface may receive power (e.g., electrical current) from power supply 140 to power the electronic properties or components.

In various embodiments, the user interface may comprise one or more components configured to receive an input from a user. For example, the user interface may comprise one or more of an audio capturing module (e.g., microphone) configured to receive an audio input, a visual display (e.g., touchscreen, LCD, LED, etc.) configured to receive a manual input, a mechanical interface (e.g., button, switch, etc.) configured to receive a manual input, and/or the like. In various embodiments, the user interface may comprise one or more components configured to transmit, provide, and/or produce an output. For example, the user interface may comprise one or more of an audio output module (e.g., audio speaker) configured to output audio, a light-emitting component (e.g., flashlight, laser guide, LED, etc.) configured to output light, a visual display (e.g., touchscreen, LCD, LED, etc.) configured to output a visual, and/or the like.

In various embodiments, projectile launcher 100 may comprise an aiming apparatus. The aiming apparatus may be coupled to a top surface of projectile launcher 100 (e.g., a top surface of handle 110 and/or a top surface of magazine 112). The aiming apparatus may comprise a telescopic sight (e.g., a scope, an optical sighting device, etc.), a red-dot sight, a holographic sight, a night vision sight, a fiber-optic sight, and/or any other suitable or desired system or apparatus to aid in aiming projectile launcher 100. The aiming apparatus may also comprise a pair of sights, including a front sight and a rear sight. In operation, a user may visually align the front sight with the rear sight to aim at a target and/or ensure projectiles P are accurately deployed.

In various embodiments, handle 110 and magazine 112 may each comprise a separate aiming apparatus. For example, handle 110 may comprise a first aiming apparatus 101 (e.g., a handle aiming apparatus, a rear sight, etc.) and magazine 112 may comprise a second aiming apparatus 102 (e.g., a magazine aiming apparatus, a front sight, etc.). First aiming apparatus 101 may be coupled to a top surface of handle 110 rearward of bay 111. Second aiming apparatus 102 may be coupled to a top surface of magazine 112. First aiming apparatus 101 and second aiming apparatus 102 may be aligned (e.g., in response to magazine 112 being coupled to handle 110). For example, first aiming apparatus 101 and second aiming apparatus 102 may be coplanar and/or colinear. First aiming apparatus 101 may be configured to visually align with second aiming apparatus 102. For example, first aiming apparatus 101 may comprise a rear sight and second aiming apparatus 102 may comprise a front sight. The rear sight may define a “U” shaped void, a “V” shaped void, or a similar rectangular shaped void. The front sight may comprise a shape complimentary to the void of the rear sight. In operation, a user may visually align the front sight within the void of the rear sight to aim projectile launcher 100 and/or to ensure projectiles P are accurately deployed.

In various embodiments, and with reference to FIGS. 2A and 2B, a magazine 212 for a projectile launcher is disclosed. Magazine 212 may be similar to any other magazine, deployment unit, or the like disclosed herein.

Magazine 212 may comprise a housing 250 (e.g., a magazine housing, a magazine body, etc.) sized and shaped to be inserted into the bay of a projectile launcher handle, as previously discussed. Housing 250 may comprise a first end 251 (e.g., a deployment end, a front end, etc.) opposite a second end 252 (e.g., a loading end, a rear end, etc.). Magazine 212 may be configured to permit launch of one or more projectiles P from first end 251 (e.g., projectiles P are launched through first end 251). Magazine 212 may be configured to permit loading of one or more projectiles P from second end 252. Second end 252 may also be configured to permit provision of electrical signals (e.g., stimulus signals, ignition signals, etc.) from the projectile launcher handle to the one or more projectiles P. Second end 252 may also be configured to permit provision of a propulsion force from the projectile launcher handle to the one or more projectiles P. In some embodiments, magazine 212 may also be configured to permit loading of one or more projectiles P from first end 251.

In various embodiments, housing 250 may define an aiming apparatus 202 (e.g., a second aiming apparatus, a magazine aiming apparatus, a front sight, etc.). Aiming apparatus 202 may be similar to any other aiming apparatus disclosed here (e.g., aiming apparatus 101, with brief reference to FIGS. 1A and 1B).

In various embodiments, second end 252 of housing 250 may define an interface (e.g., a magazine interface, a first magazine interface, etc.). The interface may be similar to any other interface disclosed herein (e.g., first magazine interface 106, with brief reference to FIGS. 1A and 1B). The interface may be configured to provide a mechanical interface and/or a fluid interface. The interface may be configured to engage with a complimentary interface of a projectile launcher handle in response to magazine 212 being coupled to the projectile launcher handle.

In various embodiments, a bottom surface of housing 250 may define an interface (e.g., a magazine interface, a second magazine interface, etc.). The interface may be similar to any other interface disclosed herein (e.g., second magazine interface 108, with brief reference to FIGS. 1A and 1B). The interface may be configured to provide a mechanical interface and/or an electrical interface. The interface may be configured to engage with a complimentary interface of a projectile launcher handle in response to magazine 212 being coupled to the projectile launcher handle.

In various embodiments, housing 250 may define one or more bores 253. A bore 253 may comprise an axial opening through housing 250, defined and open on first end 251 and/or second end 252. Each bore 253 may be configured to receive a projectile P (or a cartridge containing a projectile P). Each bore 253 may be sized and shaped accordingly to receive and house a projectile P (or a cartridge containing a projectile P) prior to and during deployment of the projectile P from magazine 212. Each bore 253 may comprise any suitable deployment angle. One or more bores 253 may comprise similar deployment angles. One or more bores 253 may comprise different deployment angles. Housing 250 may comprise any suitable or desired number of bores 253, such as, for example, two bores, four bores, eight bores (e.g., as depicted), ten bores, and/or the like.

In operation, one or more projectiles P may be inserted into one or more bores 253 of magazine 212. Magazine 212 may be inserted into the bay of a projectile launcher handle. The projectile launcher may be operated to deploy one or more projectiles P from magazine 212. Magazine 212 may be removed from the bay of the projectile launcher handle. The previously deployed one or more projectiles P (e.g., a used projectile P, a spent projectile P, etc.) may be removed from the one or more bores 253 of magazine 212. One or more new projectiles P may then be inserted into the same one or more bores 253 of magazine 212 for additional deployments. The number of projectiles P that magazine 212 is capable of receiving may be dependent on a number of bores 253 in housing 250. For example, in response to housing 250 comprising four bores 253, magazine 212 may be configured to receive at most four projectiles P at a same time. As a further example, in response to housing 250 comprising eight bores 253, magazine 212 may be configured to receive at most eight projectiles P at a same time.

In various embodiments, and with reference to FIG. 3, a propulsion module 325 is disclosed. Propulsion module 325 may be similar to, or share similar components with, any other propulsion module disclosed herein (e.g., propulsion module 125, with brief reference to FIG. 1C). Propulsion module 325 may be configured to receive a propellant from a propulsion source 330 and provide the propellant as a propulsion force to a magazine 312. For example, propulsion module 325 may be configured to receive a propellant from propulsion source 330 and distribute a propulsion force to one or more projectiles housed in magazine 312. In response to receiving the propulsion force, the one or more projectiles may be deployed from magazine 312.

In various embodiments, propulsion source 330 may comprise any suitable source of propellant. Propulsion source 330 may be similar to, or share similar components with, any other propulsion source disclosed herein (e.g., propulsion source 330, with brief reference to FIG. IC). Propulsion source 330 may be in fluid communication with one or more components of propulsion module 325. Propulsion source 330 may be configured to provide a propellant to one or more components of propulsion module 325.

In various embodiments, magazine 312 may be similar to, or share similar components with, any other magazine disclosed herein (e.g., magazine 112, with brief reference to FIGS. 1A-1C; magazine 212, with brief reference to FIGS. 2A and 2B; etc.). Magazine 312 may be configured to receive one or more projectiles. The projectiles may be similar to, or share similar components with, any other projectile disclosed herein (e.g., projectiles P, with brief reference to FIGS. 1A-2B). Magazine 312 may be in fluid communication with one or more components of propulsion module 325. In response to receiving a propulsion force from propulsion module 325, one or more projectiles may be deployed from magazine 312.

In various embodiments, propulsion module 325 may comprise one or more components configured to receive a propellant, control release of the propellant, distribute the propellant, and/or the like. For example, propulsion module 325 may comprise a valve assembly 327, an activation module 328, and/or a distribution module 350.

In various embodiments, valve assembly 327 (e.g., propulsion module valve assembly) may be configured to receive a propellant, store the propellant, and release the propellant. Valve assembly 327 may comprise any suitable valve assembly, fluid storage assembly, gas valve, gas regulator, or the like capable of receiving a propellant, storing the propellant, and release the propellant. For example, valve assembly 327 may be in fluid communication with propulsion source 330. Valve assembly 327 may be configured to receive a propellant from propulsion source 330 and store the propellant within valve assembly 327. For example, valve assembly 327 may comprise or interface with a cavity configured to store the propellant (e.g., in some embodiments, valve assembly 327 comprises a cavity and in some embodiments, valve assembly 327 interfaces with propulsion source 330 as the cavity). The cavity may be fluidly contained such that the propellant may be selectively released. Valve assembly 327 may comprise one or more valves, seals, and/or the like configured to enable the cavity to store the propellant. The one or more valves, seals, and/or the like may also be controlled to enable valve assembly 327 to release the propellant.

In various embodiments, activation module 328 (e.g., propulsion module activation module) may be configured to control release of a propellant from valve assembly 327. Activation module 328 may comprise any suitable activation mechanism, solenoid, control unit, or the like capable of controlling release of a propellant from a valve assembly. For example, activation module 328 may be in mechanical communication, electrical communication, electronic communication, and/or fluid communication with valve assembly 327. Activation module 328 may be configured to engage valve assembly 327 to cause valve assembly 327 to release a propellant. For example, activation module 328 may be configured to mechanically, electrically, electronically, and/or fluidly engage valve assembly 327 to cause valve assembly 327 to release a propellant. In that regard, activation module 328 may engage one or more valves, seals, and/or the like of valve assembly 327 to cause valve assembly 327 to release the propellant.

Activation module 328 may be controlled (e.g., activated) using any suitable process or control. For example, activation module 328 may be in electrical and/or electronic communication with a processing circuit (e.g., processing circuit 135, with brief reference to FIG. 1C). The processing circuit may transmit an electrical signal, instruction, and/or the like to activation module 328. In response to receiving the electrical signal, instruction, and/or the like, activation module 328 may engage valve assembly 327 to release a propellant stored within valve assembly 327.

In various embodiments, activation module 328 may engage valve assembly 327 for a period of time. The period of time may allow an amount of propellant to be released from valve assembly 327. The amount of propellant may be sufficient to cause deployment of one or more projectiles from magazine 312. The period of time may be based on a type of propellant, a type of projectile, a flow rate of propellant, desired deployment characteristics of a projectile (e.g., speed, velocity, distance, etc.), and/or the like. In some embodiments, the period of time may be based on a user input. In some embodiments, the period of time may be based on calculations and/or operations performed by the processing circuit.

In various embodiments, activation module 328 may comprise a solenoid. The solenoid may comprise various components, such as, for example, a housing, a translatable plunger, a wire coil, and/or the like. The solenoid may be configured to convert an electrical input into a mechanical output. For example, the solenoid may be configured to receive an electrical signal (e.g., via a processing circuit). The electrical signal may flow through the wire coil to form a magnetic field. The magnetic field may cause the translatable plunger to translate and move (e.g., change) position. In that regard, the solenoid may be configured to mechanically engage valve assembly 327. For example, the solenoid may receive an electrical signal to control operation of the solenoid. In response to receiving the electrical signal, the translatable plunger may translate and contact (e.g., touch, engage, impact, etc.) valve assembly 327 (e.g., the translatable plunger may translate from a first position into a second position). Contact of the translatable plunger may cause valve assembly 327 to release an amount of propellant, as previously discussed herein. In response to no longer receiving the electrical current, the translatable plunger may translate and return to a beginning position (e.g., the translatable plunger may translate from the second position back into the first position). In response to the translatable plunger no longer contacting valve assembly 327, valve assembly 327 may cease providing the amount of propellant.

In various embodiments, distribution module 350 (e.g., propulsion module distribution module, rotating distribution module, selective distribution module, etc.) may be configured to receive a propellant and distribute the propellant. Distribution module 350 may be in fluid communication with valve assembly 327. Distribution module 350 may be in fluid communication with magazine 312. Distribution module 350 may be in fluid communication with one or more projectiles housed in magazine 312. In that regard, distribution module 350 may be configured to receive a propellant from valve assembly 327 and provide the propellant to one or more projectiles housed in magazine 312. In response to receiving the propellant, the one or more projectiles may be launched from magazine 312.

In various embodiments, distribution module 350 may comprise any suitable component, assembly, or the like configured to provide a propellant to one or more projectiles of magazine 312. For example, distribution module 350 may comprise a fluid channel, a manifold, a cylinder, and/or the like.

In various embodiments, distribution module 350 may be configured to selectively provide propellant to one or more projectiles of magazine 312. For example, during a first deployment event (e.g., first activation event, etc.) distribution module 350 may be configured to provide propellant to a first set of projectiles; during a second deployment event distribution module 350 may be configured to provide propellant to a second set of projectiles; during a third deployment event distribution module 350 may be configured to provide propellant to a third set of projectiles; etc. Each set of projectiles may comprise one or more projectiles. Each set of projectiles may comprise different projectiles (e.g., the first set of projectiles comprises a first projectile, the second set of projectiles comprises a second projectile, the third set of projectiles comprises a third projectile, etc.).

Distribution module 350 may be configured to selectively provide propellant using any suitable process and/or components. For example, selectively providing propellant may include opening and/or closing fluid channels, directing propellant to a selected set of projectiles, and/or the like.

In various embodiments, selectively providing propellant may include adjusting (e.g., moving, rotating, translating, etc.) a fluid outlet of distribution module 350 to align with a set of projectiles. For example, during a first deployment event a fluid outlet of distribution module 350 may be aligned with a first set of projectiles (e.g., the fluid outlet is in fluid communication with the first set of projectiles). Responsive to and/or before a second deployment event the fluid outlet of distribution module 350 may be adjusted to align with a second set of projectiles (e.g., the fluid outlet is in fluid communication with the second set of projectiles). Responsive to and/or before a third deployment event the fluid outlet of distribution module 350 may be adjusted to align with a third set of projectiles (e.g., the fluid outlet is in fluid communication with the third set of projectiles).

Adjustment of distribution module 350 may include a physical movement of distribution module 350. The physical movement may include movement of distribution module 350 from a first position to a second position. As discussed further herein, the physical movement may include a rotational movement and/or a translation movement. The rotational movement may comprise a circumferential movement wherein the second position is circumferential offset from the first position. The translation movement may comprise an axial movement wherein the second position is axially offset from the first position. The rotational movement may occur before the translation movement. The rotational movement may occur before and/or during the translation movement.

Adjustment of distribution module 350 may be controlled to selectively provide propellant to various sets of projectiles. Adjustment of distribution module 350 may be controlled (e.g., activated) using any suitable process or control. Adjustment of distribution module 350 may be controlled mechanically, electrically, electronically, and/or fluidly. For example, distribution module 350 may be in electrical and/or electronic communication with a processing circuit (e.g., processing circuit 135, with brief reference to FIG. 1C). The processing circuit may transmit an electrical signal, instruction, and/or the like to distribution module 350. In response to receiving the electrical signal, instruction, and/or the like, distribution module 350 may adjust a fluid outlet of distribution module 350. As a further example, distribution module 350 may be in fluid communication with valve assembly 327. Provision of the propellant to distribution module 350 may cause distribution module 350 to adjust position (e.g., the propellant causes distribution module 350 to adjust position). As a further example, distribution module 350 may be in mechanical communication with a trigger (e.g., trigger 115, with brief reference to FIG. IC). Activation of the trigger (e.g., a manual trigger pull) may cause distribution module 350 to adjust position (e.g., the force from activating the trigger is translated to distribution module 350 to cause distribution module 350 to adjust).

In operation, and in accordance with various embodiments, propulsion module 325 may be configured to deploy, or cause deployment of, one or more projectiles in magazine 312. Propulsion source 330 may provide a propellant to valve assembly 327. Valve assembly 327 may control provision of the propellant to distribution module 350. In response to a first activation event, distribution module 350 may align with a first set of projectiles and activation module 328 may cause valve assembly 327 to provide a first amount of propellant to the first set of projectiles via distribution module 350. In response to receiving the first amount of propellant, the first set of projectiles may be deployed from magazine 312. In response to a second activation event, distribution module 350 may adjust to align with a second set of projectiles and activation module 328 may cause valve assembly 327 to provide a second amount of propellant to the second set of projectiles via distribution module 350. In response to receiving the second amount of propellant, the second set of projectiles may be deployed from magazine 312. This process may continue as desired by a user, until all projectiles are deployed, until propulsion source 330 is depleted of propellant, and/or the like. In some embodiments, new projectiles may be loaded in magazine 312 and/or a new propulsion source 330 may be provided to continue the process.

In various embodiments, distribution module 350 may comprise, or be a component of, a fluid interface of a projectile launcher handle. In that regard, distribution module 350 may be coupled to an inner surface of a projectile launcher handle proximate a bay of the projectile launcher handle. Distribution module 350 may be positioned within the bay of the projectile launcher handle such that distribution module 350 may interface with magazine 312 to selectively provide propellant to one or more projectiles of magazine 312. For example, a forward surface of distribution module 350 may extend through (or be accessible via) the bay of the projectile launcher handle. In some embodiments, distribution module 350 may engage a fluid interface (e.g., a magazine fluid interface) of magazine 312.

In various embodiments, and with reference to FIGS. 4A-4D, a distribution module 450 is disclosed. Distribution module 450 may be similar to, or share similar components with, any other distribution module disclosed herein (e.g., distribution module 350, with brief reference to FIG. 3). Distribution module 450 may be configured to rotate to adjust position for selectively providing propellant, as discussed further herein.

In various embodiments, distribution module 450 may comprise one or more components, structures, and/or the like that rotate and one or more components, structures, and/or the that remain stationary and do not rotate. For example, distribution module 450 may comprise a static outer housing 460, a rotating inner housing 455, and/or the like. Static outer housing 460 and rotating inner housing 455 may share a common axis. Static outer housing 460 and rotating inner housing 455 may be colinear.

In various embodiments, static outer housing 460 may comprise one or more static components, structures, and/or the like that remain stationary. Rotating inner housing 455 may comprise one or more rotating components, structures, and/or the like. In that regard, in response to distribution module 450 adjusting position to selectively providing propellant, rotating inner housing 455 may rotate while static outer housing 460 remains stationary.

In various embodiments, static outer housing 460 may comprise a body (e.g., a static outer housing body) having a first end 461 (e.g., first static outer housing end) opposite a second end 462 (e.g., second outer housing end). First end 461 may define a forward surface or edge of static outer housing 460. Second end 462 may define a rear surface or edge of static outer housing 460. The body of static outer housing 460 may define an opening 463 (e.g., a static outer housing opening). Opening 463 may be defined on first end 461, through the body of static outer housing 460, and on second end 462.

In some embodiments, opening 463 may comprise a varying diameter. For example, opening 463 on first end 461 may comprise a greater diameter than opening 463 at second end 462. In that regard, second end 462 may comprise a lipped surface extending radially inward from an outer circumferential edge of the body of static outer housing 460. The lipped surface may define the small diameter opening 463 on second end 462.

In various embodiments, opening 463 may be sized and shaped to receive one or more components, structures, and/or the like of rotating inner housing 455. Opening 463 at first end 461 may be sized and shaped to receive one or more components, structures, and/or the like of rotating inner housing 455. For example, and as discussed further herein, opening 463 at first end 461 may be configured to receive (fully or at least partially) a cylindrical body 480 of rotating inner housing 455. Opening 463 at first end 461 may comprise a shape that is complimentary with cylindrical body 480. Opening 463 at second end 462 may be sized and shaped to receive one or more components, structures, and/or the like of rotating inner housing 455. For example, and as discussed further herein, opening 463 at second end 462 may be configured to receive (fully or at least partially) a rotational gear and/or an inlet of rotating inner housing 455.

In various embodiments, static outer housing 460 may be configured to mount to an inner surface of a projectile launcher handle. For example, a top surface of static outer housing 460 between first end 461 and second end 462 may be configured to couple to an inner surface of a projectile launcher handle. Static outer housing 460 may be configured to mount to any suitable location within a projectile launcher handle. Static outer housing 460 may be configured to mount to an inner surface proximate a top surface of the projectile launcher handle. Static outer housing 460 may be configured to mount to an inner surface proximate a bay of a projectile launcher handle. Static outer housing 460 may be configured to mount to an inner surface proximate the bay such that a portion of distribution module 450 extends through, or is accessible via, the bay.

In various embodiments, static outer housing 460 may comprise any suitable shape. Static outer housing 460 may comprise a shape complimentary with a shape of rotating inner housing 455. Static outer housing 460 may comprise a cylindrical shape. Static outer housing 460 may comprise a conical shape.

In various embodiments, rotating inner housing 455 may comprise a cylindrical body 480, a rotational gear 490, and/or an inlet 470. Cylindrical body 480, rotational gear 490, and/or inlet 470 may share a common axis. Cylindrical body 480, rotational gear 490, and/or inlet 470 may be colinear.

In various embodiments, cylindrical body 480 may comprise a first end 481 (e.g., first cylindrical body end, first rotating inner housing end, first distribution module end, etc.) opposite a second end 482 (e.g., second cylindrical body end). First end 481 may define a forward surface of cylindrical body 480. Second end 482 may define a rear surface of cylindrical body 480. Cylindrical body 480 may be disposed (fully or at least partially) within static outer housing 460. For example, cylindrical body 480 may be sized and shaped to fit within opening 463 of static outer housing 460. In that regard, cylindrical body 480 may rotate within opening 463 of static outer housing 460 while static outer housing 460 remains stationary.

In some embodiments, cylindrical body 480 may comprise a varying diameter. For example, first end 481 may comprise a greater diameter than second end 482. The varying diameter of cylindrical body 480 may be complimentary to the varying diameter of opening 463 of static outer housing 460. In that regard, second end 482 may be configured to be received (fully or at least partially) within the lipped surface of second end 462 of static outer housing 460.

In various embodiments, cylindrical body 480 may define a channel 487 (e.g., fluid channel, cylindrical body channel, distribution channel, etc.). Channel 487 may extend from second end 482 through to first end 481. Channel 487 may be configured to receive and distribute a propellant. For example, channel 487 may define an outlet 485 (e.g., fluid outlet, cylindrical body outlet, distribution outlet, etc.) on first end 481. In that regard, channel 487 may receive a propellant at second end 482 and may distribute the propellant at outlet 485 of first end 481. Outlet 485 may be configured to provide a fluid interface to a magazine and/or a projectile housed in the magazine. Outlet 485 may be sized and shaped to distribute an amount of propellant to the projectile. For example, outlet 485 may be aligned with a projectile and/or a bore in a magazine in response to the magazine being coupled to a projectile launcher handle housing distribution module 450 (e.g., during operation of a projectile launcher).

In some embodiments, outlet 485 may comprise a size and shape complimentary to a projectile. In that regard, outlet 485 may at least partially receive an end of a projectile during operation of a projectile launcher. Outlet 485 may provide the amount of propellant to the projectile. Outlet 485 may fluidly seal around the projectile.

In some embodiments, outlet 485 may comprise a size and shape complimentary to a bore of a magazine. In that regard, outlet 485 may be configured to align with and/or seal against a bore of a magazine during operation of a projectile launcher. Outlet 485 may provide the amount of propellant to the bore of the magazine. Outlet 485 may fluidly seal around the bore of the magazine.

Although depicted in FIGS. 4A-4D comprising a single channel and a single outlet, in various embodiments cylindrical body 480 may comprise any suitable and/or desired number of channels and/or outlets. For example, cylindrical body 480 may comprise a single channel fluidly connected to a plurality of outlets. As a further example, cylindrical body 480 may comprise a plurality of channels with each channel fluidly connected to a separate outlet. Cylindrical body 480 may comprise a number of outlets equaling a number of projectiles to be deployed at a same time. For example, cylindrical body 480 may comprise two outlets. Each outlet may be aligned with a separate projectile. During an activation event, propellant may be provided through each outlet to deploy the two separate projectiles. Further, each outlet may be arranged on first end 481 in any suitable pattern or arrangement. For example, a plurality of outlets may be proximate each other on first end 481. A plurality of outlets may be distal each other on first end 481.

In various embodiments, cylindrical body 480 may comprise any suitable shape. Cylindrical body 480 may comprise a shape complimentary with a shape of static outer housing 460. For example, cylindrical body 480 may comprise a shape complimentary with opening 463 of static outer housing 460. Cylindrical body 480 may comprise a cylindrical shape, a conical shape, and/or any other suitable or desired shape.

In various embodiments, rotational gear 490 may comprise a first end 491 (e.g., first rotational body end) opposite a second end 492 (e.g., second rotational body end, second rotating inner housing end, second distribution module end, etc.). First end 491 may define a forward surface of rotational gear 490. First end 491 may be coupled to second end 482 of cylindrical body 480. Second end 492 may define a rear surface of rotational gear 490. Second end 492 may be coupled to inlet 470, as discussed further herein. Rotational gear 490 may define an opening 493 (e.g., a rotational gear opening, a rotational gear channel, etc.) extending through rotational gear 490. Opening 493 may be defined on first end 491 and second end 492.

In various embodiments, opening 493 may be configured, and sized and shaped, to provide a fluid (e.g., propellant) to channel 487 of cylindrical body 480. First end 491 may define an axial protrusion circumferentially defining opening 493. The axial protrusion may be configured to couple within opening 463 of static outer housing 460. In that regard, the axial protrusion may be coupled within opening 493 of rotational gear 490 to fluidly couple opening 493 of rotational gear 490 with channel 487 of cylindrical body 480 (e.g., the axial protrusion may insert within second end 482 of cylindrical body 480). The axial protrusion may also be inserted through opening 463 of static outer housing 460. The axial protrusion may be configured to at least partially fluidly seal the fluid coupling between channel 487 of cylindrical body 480 and opening 493 of rotational gear 490. As discussed further herein, opening 493 at second end 492 may be configured, and sized and shaped, to receive a portion of inlet 470. In that regard, opening 493 may fluidly couple channel 487 of cylindrical body 480 with inlet 470 (e.g., fluid may be provided via inlet 470 and through opening 493 to channel 487).

In various embodiments, rotational gear 490 may be configured to rotate and cause rotation of cylindrical body 480. For example, rotational gear 490 may be coupled to cylindrical body 480. In response to rotational gear 490 rotating, cylindrical body 480 may similarly rotate. In that regard, rotational gear 490 may control rotation of cylindrical body 480. Controlling rotation of cylindrical body 480 may control position of channel 487 and alignment of outlet 485 of cylindrical body 480, which may control selection of one or more projectiles for deployment.

In various embodiments, rotational gear 490 may comprise any suitable shape. Rotational gear 490 may comprise a shape complimentary with a shape of cylindrical body 480. Cylindrical body 480 may comprise a cylindrical shape, a conical shape, and/or any other suitable or desired shape. Rotational gear 490 may comprise a gear shape. Rotational gear 490 may comprise one or more structures, components, features, or the like configured to enable rotation of rotational gear 490. Rotational gear 490 may comprise one or more structures, components, features, or the like configured to fix rotational gear 490 into a position during or responsive to a rotation.

In various embodiments, rotational gear 490 may comprise one or more axial teeth 497. Axial teeth 497 may extend axially rearward from second end 492 of rotational gear 490. Axial teeth 497 may be positioned circumferentially around, or proximate to, opening 493. Axial teeth 497 may be evenly distributed and separated on second end 492 around opening 493. Axial teeth 497 may be distributed and offset unevenly on second end 492 around opening 493. Axial teeth 497 may comprise any suitable shape and/or structure. For example, axial teeth 497 may comprise a ramp shape, a rectangular shape, a square shape, and/or the like. In some embodiments, axial teeth 497 may be positioned proximate to, or in circumferentially surrounding, inlet 470.

In various embodiments, axial teeth 497 may be configured to enable rotational gear 490 to rotate. Axial teeth 497 may be configured to rotate, or cause rotation of, rotational gear 490. Rotating, or causing rotation of, rotational gear 490 may also cause rotation of cylindrical body 480 (and distribution module 450 by extension). Axial teeth 497 may rotate, or cause rotation of, rotational gear 490 in any suitable direction. For example, axial teeth 497 may rotate, or cause rotation of, rotational gear 490 in a clockwise direction. As a further example, axial teeth 497 may rotate, or cause rotation of, rotational gear 490 in a counterclockwise direction. As a further example, axial teeth 497 may rotate, or cause rotation of, rotational gear 490 into one or more positions (e.g., distribution position, rotational position, etc.). For example, axial teeth 497 may be configured to rotate, or cause rotation of, rotational gear 490 into a first position (e.g., a first rotational position), a second position (e.g., a second rotational position), a third position (e.g., a third rotational position), etc. The number of positions (e.g., rotational positions) may be based on any suitable factor. For example, a number of positions may be based on a number of projectiles to be deployed, a number of bores in an associated magazine, a number of axial teeth 497, and/or the like.

In various embodiments, rotational gear 490 may comprise any suitable number of axial teeth 497. A number of axial teeth 497 may be associated with or based on a number of positions that cylindrical body 480 is configured to rotate into. For example, as previously discussed outlet 485 may be configured to provide a propellant to an associated projectile and/or magazine to launch the projectile. Cylindrical body 480 may rotate to cause outlet 485 to align with a next projectile. In that regard, cylindrical body 480 may be configured to rotate into a plurality of positions (e.g., rotational positions), with each position aligning outlet 485 with a different projectile. For example, in response to cylindrical body 480 being configured to rotate into 8 position, rotational gear 490 may comprise 8 axial teeth 497. In response to cylindrical body 480 being configured to rotate into 4 positions, rotational gear 490 may comprise 4 axial teeth 497.

In various embodiments, a number of axial teeth 497 may be associated with or based on a number of projectiles configured to be deployed by an associated projectile launcher. For example, in response to outlet 485 of cylindrical body 480 being configured to launch a single projectile at a same time and the number of projectiles comprising 8 projectiles, rotational gear 490 may comprise 8 axial teeth 497. In response to outlet 485 of cylindrical body 480 being configured to launch two projectiles at a same time and the number of projectiles comprising 8 projectiles, rotational gear 490 may comprise 4 axial teeth 497.

In various embodiments, a number of axial teeth 497 may be associated with or based on a number of bores of an associated magazine of a projectile launcher. For example, in response to outlet 485 of cylindrical body 480 being configured to align with a single bore at a same time and the number of bores comprising 8 bores, rotational gear 490 may comprise 8 axial teeth 497. In response to outlet 485 of cylindrical body 480 being configured to align with two bores at a same time and the number of bores comprising 8 bores, rotational gear 490 may comprise 4 axial teeth 497.

In various embodiments, and as discussed further herein, a number of axial teeth 497 may be associated with or based on a number of radial teeth 496. In that regard, a number of axial teeth 497 may be the same as a number of radial teeth 496 (e.g., a rotational gear comprising 8 radial teeth may also comprise 8 axial teeth). In other embodiments, a number of axial teeth 497 may be double a number of radial teeth 496 (e.g., a rotational gear comprising 4 radial teeth may also comprise 8 axial teeth), half a number of radial teeth 496 (e.g., a rotational gear comprising 8 radial teeth may also comprise 4 axial teeth), and/or the like.

In various embodiments, one or more components, structures, assemblies, or the like of a projectile launcher (collectively, a “projectile launcher assembly”) may be configured to engage axial teeth 497 to rotate, or cause rotation of, rotational gear 490. For example, a projectile launcher assembly may engage a lower surface of one or more axial teeth 497. The projectile launcher assembly may apply a force (e.g., a radial force) against the lower surface of the one or more axial teeth 497. The force may cause the one or more axial teeth 497 (and by extension rotational gear 490) to rotate in a direction (e.g., clockwise direction, counterclockwise direction, etc.).

In various embodiments, rotational gear 490 may comprise one or more radial teeth 496. Radial teeth 496 may extend radially outward from a circumferential edge of rotational gear 490. Radial teeth 496 may be positioned circumferentially around rotational gear 490. Radial teeth 496 may be evenly distributed and separated along the circumferential edge of rotational gear 490. Radial teeth 496 may be distributed and offset unevenly along the circumferential edge of rotational gear 490. Radial teeth 496 may comprise any suitable shape and/or structure. For example, radial teeth 496 may comprise a triangular shape, a gear-tooth shape, a ramp shape, a rectangular shape, and/or the like. In some embodiments, radial teeth 496 may be positioned proximate to, or in contact with, second end 462 of static outer housing 460.

In various embodiments, radial teeth 496 may be configured to fix (e.g., place, position, etc.) rotational gear 490 into one or more positions (e.g., distribution position, rotational position, etc.). Fixing rotational gear 490 into a position may also fix cylindrical body 480 (and distribution module 450 by extension) into a position. For example, as previously discussed rotational gear 590 may be configured to rotate in a direction. Rotational gear 490 may be configured to rotate into one or more positions. In response to rotational gear 490 being rotated into a position, or based on rotation of rotational gear 490 into the position, radial teeth 496 may be configured to fix rotational gear 490 in the position. Radial teeth 496 may be configured to fix cylindrical body into a first position, a second position, a third position, etc. The number of positions may be based on any suitable factor. For example, a number of positions may be based on a number of projectiles to be deployed, a number of bores in an associated magazine, a number of radial teeth 496, and/or the like.

In various embodiments, rotational gear 490 may comprise any suitable number of radial teeth 496. A number of radial teeth 496 may be associated with or based on a number of positions that cylindrical body 480 is configured to rotate into. For example, as previously discussed outlet 485 may be configured to provide a propellant to an associated projectile and/or magazine to launch the projectile. Cylindrical body 480 may rotate to cause outlet 485 to align with a next projectile. In that regard, cylindrical body 480 may be configured to rotate into a plurality of positions, with each position aligning outlet 485 with a different projectile. For example, in response to cylindrical body 480 being configured to rotate into 8 positions, rotational gear 490 may comprise 8 radial teeth 496. In response to cylindrical body 480 being configured to rotate into 4 positions, rotational gear 490 may comprise 4 radial teeth 496.

In various embodiments, a number of radial teeth 496 may be associated with or based on a number of projectiles configured to be deployed by an associated projectile launcher. For example, in response to outlet 485 of cylindrical body 480 being configured to launch a single projectile at a same time and the number of projectiles comprising 8 projectiles, rotational gear 490 may comprise 8 radial teeth 496. In response to outlet 485 of cylindrical body 480 being configured to launch two projectiles at a same time and the number of projectiles comprising 8 projectiles, rotational gear 490 may comprise 4 radial teeth 496.

In various embodiments, a number of radial teeth 496 may be associated with or based on a number of bores of an associated magazine of a projectile launcher. For example, in response to outlet 485 of cylindrical body 480 being configured to align with a single bore at a same time and the number of bores comprising 8 bores, rotational gear 490 may comprise 8 radial teeth 496. In response to outlet 485 of cylindrical body 480 being configured to align with two bores at a same time and the number of bores comprising 8 bores, rotational gear 490 may comprise 4 radial teeth 496.

In various embodiments, and as discussed further herein, a number of radial teeth 496 may be associated with or based on a number of axial teeth 497. In that regard, a number of radial teeth 496 may be the same as a number of axial teeth 497 (e.g., a rotational gear comprising 8 axial teeth may also comprise 8 radial teeth). In other embodiments, a number of radial teeth 496 may be double a number of axial teeth 497 (e.g., a rotational gear comprising 4 axial teeth may also comprise 8 radial teeth), half a number of axial teeth 497 (e.g., a rotational gear comprising 8 axial teeth may also comprise 4 radial teeth), and/or the like.

In various embodiments, one or more radial teeth 496 may structurally align with one or more axial teeth 497. One or more radial teeth 496 may be colinear with one or more axial teeth 497. For example, a first radial teeth may be colinear with a first axial teeth, a second radial teeth may be colinear with a second axial teeth, and/or the like. Radial teeth 496 may be located proximate axial teeth 497. Radial teeth 496 may be radially outward from axial teeth 497. Axial teeth 497 may be radially inward from radial teeth 496. Axial teeth 497 may be located between radial teeth 496 and opening 493.

In some embodiments, radial teeth 496 may extend in a first direction and axial teeth 497 may extend in a second direction. The first direction may be different from the second direction. The first direction may be perpendicular to the second direction. The first direction may comprise a radial direction and the second direction may comprise an axial direction. The first direction may comprise an upward direction and the second direction may comprise a rearward direction.

In various embodiments, one or more components, structures, assemblies, or the like of a projectile launcher (collectively, a “projectile launcher assembly”) may be configured to engage radial teeth 496 to fix rotational gear 490 into a position. For example, a projectile launcher assembly may engage an outer surface of one or more radial teeth 496. The projectile launcher assembly may apply a force (e.g., a radial force) against the outer surface of the one or more radial teeth 496. The force may cause the one or more radial teeth 496 (and by extension rotational gear 490) to be fixed in a position.

In various embodiments, distribution module 450 may comprise a position tab 465. Position tab 465 may be configured to fix rotational gear 490 into a position (e.g., rotational position). Position tab 465 may be configured to cooperate with radial teeth 496 to fix rotational gear 490 into a position. In that regard, the projectile launcher assembly previously discussed configured to engage radial teeth 496 may comprise one or more position tabs 465. Position tab 465 may be configured to engage (e.g., contact, interfere, position, etc.) one or more radial teeth 496 to fix rotational gear 490 into a position. For example, position tab 465 may apply a force (e.g., a radial force) against an outer surface of one or more radial teeth 496. The force may cause the one or more radial teeth 496 (and by extension rotational gear 490) to be fixed in a position.

In various embodiments, position tab 465 may be coupled to any suitable location within a projectile launcher capable of allowing position tab 465 to engage one or more radial teeth 496. For example, position tab 465 may be coupled to static outer housing 460. Position tab 465 may be coupled to static outer housing 460 proximate a top end of static outer housing 460. Position tab 465 may be coupled to static outer housing 460 at a location proximate to or at second end 462 of static outer housing 460. Position tab 465 may be coupled to static outer housing 460 at a location proximate rotational gear 490. Position tab 465 may be coupled to static outer housing 460 at a location proximate one or more radial teeth 496.

In various embodiments, position tab 465 may comprise any suitable size or shape. Position tab 465 may comprise a size and shape capable of allowing position tab 465 to engage one or more radial teeth 496. For example, position tab 465 may comprise a triangular shape, a rectangular shape, a square shape, and/or the like. Position tab 465 may comprise a varying width (e.g., a top portion of position tab 465 is wider than a bottom portion of position tab 465; a bottom portion of position tab 465 is wider than a top portion of position tab 465; a middle portion of position tab 465 is wider than at least one of a top portion or a bottom portion of position tab 465; at least one of a top portion or a bottom portion of position tab 465 is wider than a middle portion of position tab 465; etc.).

In various embodiments, position tab 465 may comprise any suitable material. For example, position tab 465 may comprise a spring, a metal, and/or the like. Position tab 465 may comprise a material that flexes in response to receiving a force in an axial direction (e.g., against a forward surface or rearward surface of position tab 465). Position tab 465 may comprise a material that remains stiff in response to receiving a force in a radial direction (e.g., against a bottom surface of position tab 465). In that regard, position tab 465 may be configured to flex in response to receiving a force against a forward surface or rearward surface of position tab 465, but remain stiff in response to receiving a force against a bottom surface of position tab 465. For example, during rotation of rotational gear 490, a first surface (e.g., a left surface) of a radial teeth may contact a rearward surface of position tab 465. Position tab 465 may flex in an opposite direction to allow the radial teeth to continue rotating. In response to rotational gear 490 being rotated into a desired position, a bottom surface of position tab 465 may contact a second surface (e.g., a right surface) of the radial teeth. Position tab 465 may remain stiff (e.g., apply a force) against the second surface of the radial teeth to fix rotational gear 490 into the position. In that respect, position tab 465 may cooperate with radial teeth 496 to fix rotational gear 490 into a position.

In various embodiments, inlet 470 may comprise a first end 471 (e.g., first inlet end) opposite a second end 472 (e.g., second inlet end). First end 471 may define a forward surface or edge of inlet 470. Second end 472 may define a rear surface or edge of inlet 470. First end 471 may be configured to couple to one or more of static outer housing 460, cylindrical body 480, and/or rotational gear 490. Second end 472 may be configured to couple to a propulsion source, such as a valve assembly (e.g., valve assembly 327, with brief reference to FIG. 3). In that regard, inlet 470 may receive a propellant at second end 472 and may deliver the propellant at first end 471 to one or more other components of distribution module 450.

In various embodiments, inlet 470 may comprise a varying diameter. For example, second end 472 may comprise a greater diameter than first end 471. The varying diameter of inlet 470 may be complimentary to one or more of opening 493 of rotational gear 490, opening 463 of static outer housing 460, and/or an opening of channel 487 of cylindrical body 480. In that regard, a portion of first end 471 of inlet 470 comprising a smaller diameter may be configured to be inserted (fully or at least partially) within one or more of opening 493 of rotational gear 490, opening 463 of static outer housing 460, and/or an opening of channel 487 of cylindrical body 480.

In some embodiments, an outer surface of first end 471 may be configured to engage an inner surface of opening 493 of rotational gear 490. The outer surface of first end 471 may be configured to engage the inner surface of opening 493 of rotational gear 490 to at least partially fluidly seal the fluid coupling between inlet 470 and rotational gear 490. Fluidly sealing the fluid coupling may ensure that fluid provided to second end 472 of inlet 470 may travel through to channel 487 of cylindrical body 480 without (or with a decreased amount of) fluid loss.

In various embodiments, inlet 470 may define an opening 473 (e.g., an inlet opening, a distribution module inlet, etc.). Opening 473 may be defined on first end 471, through the body of inlet 470, and on second end 472. Opening 473 may be in fluid communication with one or more of opening 493 of rotational gear 490, opening 463 of static outer housing 460, and/or channel 487 of cylindrical body 480. Opening 473 may be configured, and sized and shaped, to provide a fluid (e.g., propellant) to channel 487 of cylindrical body 480. For example, opening 473 may provide the fluid to channel 487 directly or via opening 493 of rotational gear 490 and/or opening 463 of static outer housing 460.

In various embodiments, inlet 470 may be configured to rotate responsive to rotation of rotational gear 490. In that regard, inlet 470 may be coupled to rotational gear 490 and/or cylindrical body 480. For example, first end 471 of inlet 470 may be coupled within an opening of rotational gear 490 and/or cylindrical body 480.

In various embodiments, inlet 470 may be configured to remain stationary responsive to rotation of rotational gear 490. In that regard, inlet 470 may be coupled to static outer housing 460 and/or a propulsion source, such as a valve assembly (e.g., valve assembly 327, with brief reference to FIG. 3). For example, first end 471 of inlet 470 may be coupled within an opening of 463 of static outer housing 460 and/or second end 472 of inlet 470 may be coupled to the propulsion source, such as the valve assembly.

In various embodiments, and with reference to FIGS. 5A and 5B, distribution module 450 is depicted in a first position (e.g., first rotational position). Position tab 465 may contact a radial teeth 496 (e.g., a first radial teeth) to fix rotational gear 490 into the first position. In the first position, channel 487 and outlet 485 may be configured to provide a propellant to a first set of projectiles comprising one or more projectiles, as previously discussed herein. In that regard, outlet 485 may be aligned with a magazine such that propellant is provided from outlet 485 to the first set of projectiles. The propellant may be provided from a propellant source (e.g., directly or via a valve assembly), through inlet 470, rotational gear 490 and/or static outer housing 460, and channel 487, and out outlet 485 to the first set of projectiles.

In various embodiments, and with reference to FIGS. 6A and 6B, distribution module 450 is depicted in a next position (e.g., a next rotational position). The next position may be different from the first position. The next position may comprise a second position relative to the first position in which distribution module 450 is depicted in FIGS. 5A and 5B. Distribution module 450 may rotate from a previous position, such as the first position depicted in FIGS. 5A and 5B, to the next position. Rotation of distribution module 450 may comprise rotation of a portion of distribution module 450. For example, rotation of distribution module 450 may comprise rotation of cylindrical body 480. Rotation of distribution module 450 may comprise maintaining another portion of distribution module 450 in a fixed position. For example, rotation of distribution module 450 may comprise maintaining static outer housing 460 in a fixed position within a projectile launcher while cylindrical body 480 is rotated. Rotation of distribution module 450 may be responsive to engagement and force applied to an axial teeth 497 (e.g., a next axial teeth) of rotational gear 490. Position tab 465 may contact a radial teeth 496 (e.g., a next radial teeth) of rotational gear 490 to fix rotational gear 490 into the next position. In the next position, channel 487 and outlet 485 may be configured to provide a propellant to a next set of projectiles comprising one or more projectiles, as previously discussed herein. The next set of projectiles may be different than the first set of projectiles. In that regard, outlet 485 may be aligned with a magazine such that propellant is provided from outlet 485 to the next set of projectiles. The propellant may be provided from a propellant source (e.g., directly or via a valve assembly), through inlet 470, rotational gear 490 and/or static outer housing 460, and channel 487, and out outlet 485 to the next set of projectiles. An angular position of outlet 485 about an axis of rotation of distribution module 450 may change between the first position and the next position. Rotation of distribution module 450 may cause an angular displacement of outlet 485. A location of outlet 485 when distribution module 450 is disposed in the first position may be different from a location of outlet 485 when distribution module 450 is disposed in the next position. In contrast, a position of opening 473 may remain fixed between the first position and the next position. Independent of whether inlet 470 is configured to rotate or remain fixed between the first position and the next position, a location of opening 473 may be maintained when distribution module 450 is disposed in each of the first position and the next position. The location of opening 473 may be disposed along the axis of rotation in each of the first position and the next position. Such an arrangement may enable a valve assembly coupled to inlet 470 to remain in a fixed location within a projectile launcher, yet provide propellant via distribution module 450 to different relative locations within the projectile launcher at which different projectiles may be disposed.

In various embodiments, and with reference to FIGS. 7A and 7B, a control assembly 754 (e.g., trigger control assembly, projectile launcher assembly, etc.) is disclosed. Control assembly 754 may be configured to control operation of distribution module 450. For example, control assembly 754 may be configured to control a rotation of distribution module 450, a position of distribution module 450, and/or the like. Controlling rotation, position, and/or the like of distribution module 450 may control selection of one or more sets of projectiles for deployment. Control assembly 754 may engage one or more components of distribution module 450 to control rotation, position, and/or the like of distribution module 450, as discussed further herein.

In various embodiments, control assembly 754 may comprise a control arm 720, a translatable member 716, and/or a biasing member 729. Control arm 720 may be configured to control operation of distribution module 450. Control arm 720 may be configured to receive a first force and provide a second force to control operation of distribution module 450. In some embodiments, the first force may be the same as the second force. For example, the first force may comprise a radially upward movement and the second force may comprise a radially upward movement. In some embodiments, the first force may be different from the second force. For example, the first force may comprise a translatable force including an axial movement (e.g., movement in an axial direction) and the second force may comprise a radially upward movement.

Control arm 720 may comprise a first end 721 (e.g., first control arm end) opposite a second end 722 (e.g., second control arm end). First end 721 may be configured to engage distribution module 450. For example, first end 721 may be configured to engage (e.g., contact, interface, etc.) rotational gear 490. First end 721 may be configured to engage one or more axial teeth 497 of rotational gear 490. In that regard, first end 721 may be configured to engage a lower surface (e.g., bottom surface) of an axial teeth 497. First end 721 may be configured to apply a force to the lower surface of the axial teeth 497. Movement of control arm 720 may cause first end 721 to provide the force to the lower surface of the axial teeth 497. Application of the force may cause rotational gear 490 to rotate, as previously discussed herein. First end 721 may comprise any suitable shape capable of engaging distribution module 450. For example, first end 721 may comprise an elongated surface extending axially forward toward distribution module 450. First end 721 may comprise a rectangular shape, a triangular shape, and/or the like. First end 721 may comprise a boot shape, a ramp shape, and/or the like.

Second end 722 may be coupled to translatable member 716 and/or a trigger 715. Trigger 715 may be similar to, or share similar components with, any other trigger disclosed herein (e.g., trigger 115, with brief reference to FIGS. 1A-1C). Second end 722 may receive a force responsive to movement of translatable member 716 and/or trigger 715. The force received at second end 722 may cause movement of control arm 720, such as, for example, movement of control arm 720 in a radially upward direction. In various embodiments, activation of trigger 715 may cause movement of translatable member 716 and/or trigger 715. Activation of trigger 715 may cause trigger 715 to pivot about an axis. For example, trigger 715 may pivot about an axis such that a rear end of trigger 715 moves axially rearward while an upper rear end of trigger 715 moves radially upward. Movement of trigger 715 may cause movement of translatable member 716. Movement of trigger 715 and/or translatable member 716 may apply the force to second end 722.

Second end 722 may comprise any suitable shape capable of coupling to translatable member 716 and/or trigger 715. For example, second end 722 may comprise an elongated surface extending radially outward from second end 722 and towards translatable member 716 and/or trigger 715. Second end 722 may comprise a rectangular shape, a square shape, a triangular shape, a circular shape and/or the like. Second end 722 may comprise a peg-shaped extension. In that regard, a portion of second end 722 may be insertable into a portion of translatable member 716, as discussed further herein.

In various embodiments, translatable member 716 may be configured to provide (e.g., translate) movement from trigger 715 to control arm 720. In that regard, translatable member 716 may receive a movement from trigger 715 and provide a force (e.g., a movement) to control arm 720. Translatable member 716 may comprise a first end 718 (e.g., first translatable member end) opposite a second end 719 (e.g., second translatable member end). Second end 719 may be coupled to trigger 715. First end 718 may be coupled to second end 722 of control arm 720. For example, first end 718 may define an aperture (e.g., translatable member aperture). A portion (e.g., a peg-shaped extension) of second end 722 of control arm 720 may be inserted within the aperture to couple first end 718 to second end 722 of control arm 720. The aperture of first end 718 may comprise a surface area larger than the portion of second end 722 of control arm 720 inserted within the aperture. In that respect, the portion of second end 722 of control arm 720 inserted within the aperture may move within the aperture. Movement within the aperture may be responsive to activation of trigger 715, as discussed further herein.

In various embodiments, biasing member 729 may be configured to provide a biasing force against control arm 720. The biasing force may comprise a force in an axially forward direction. The biasing force may be configured to bias control arm 720 against rotational gear 490. The biasing force may allow control arm 720 to cause rotation of rotational gear 490. For example, the biasing force may allow first end 721 of control arm 720 to contact one or more axial teeth 497. The biasing force may position first end 721 of control arm 720 against a lower surface of an axial teeth 497. Control arm 720 may apply a force (e.g., a radially upward force) against the lower surface of the axial teeth 497 to rotate rotational gear 490. Subsequent to rotation, control arm 720 may move radially downward causing control arm 720 to no longer rotate rotational gear 490. The biasing force may allow first end 721 of control arm 720 to contact and pass over one or more axial teeth 497 during the radially downward movement. After passing over the one or more axial teeth 497, the biasing force may again position first end 721 of control arm 720 in contact with a lower surface of a next axial teeth 497.

In various embodiments, and with reference to FIGS. 8A-8C, operation of control assembly 754 is depicted. With specific reference to FIG. 8A, control assembly 754 is depicted in a first control position. In the first control position, trigger 715 has not been activated. Second end 722 of control arm 720 is inserted within an aperture of second end 719 of translatable member 716. Second end 722 of control arm 720 may be positioned within a forward or middle portion of the aperture of second end 719 of translatable member 716. First end 721 of control arm 720 is positioned in contact with a lower surface of a first axial teeth 897-1. Position tab 465 may be in contact with a first radial teeth 896-1 to fix distribution module 450 into a first deployment position.

With specific reference to FIG. 8B, control assembly 754 is depicted in a second control position. In the second control position, an activation of trigger 715 has begun (e.g., depressed, pulled, etc.). Movement of trigger 715 may cause movement of control arm 720 in a radially upward direction. For example, movement of trigger 715 may cause translation of translatable member 716. Translation of translatable member 716 may cause second end 722 of control arm 720 to move within a middle portion or rearward portion of the aperture of second end 719 of translatable member 716. Movement of second end 722 of control arm 720 may cause control arm 720 to move in a radially upward direction. First end 721 of control arm 720 may apply a radially upward force against the lower surface of first axial teeth 897-1. The radially upward force may cause rotational gear 490 to rotate in a counterclockwise direction. The rotation in the counterclockwise direction may rotate first radial teeth 896-1 out of contact with position tab 465. The rotation in the counterclockwise direction may rotate distribution module 450 into a second deployment position.

With specific reference to FIG. 8C, control assembly 754 is depicted in a third control position. In the third control position, trigger 715 has been activated and released. Position tab 465 may be in contact with a second radial teeth 896-2 to fix distribution module 450 into the second deployment position. The release of trigger 715 may cause trigger 715 to move and return to a starting position (e.g., as depicted in FIG. 8A). Movement of trigger 715 may cause movement of control arm 720 in a radially downward direction. For example, movement of trigger 715 may cause translation of translatable member 716. Translation of translatable member 716 may cause second end 722 of control arm 720 to move within a middle portion or forward portion of the aperture of second end 719 of translatable member 716. Movement of second end 722 of control arm 720 may cause control arm 720 to move in a radially downward direction. First end 721 of control arm 720 may move radially downward from first axial teeth 897-1 and towards a second axial teeth 897-2. Biasing member 729 may apply a biasing force against control arm 720 such that control arm 720 may contact and move over second axial teeth 897-2.

In various embodiments, after the third control position control assembly 754 may be operated back into the first control position. In the first control position, first end 721 of control arm 720 may now be positioned in contact with a lower surface of second axial teeth 897-2. Position tab 465 may remain in contact with second radial teeth 896-2 to fix distribution module 450 into the second deployment position.

In various embodiments, control assembly 754 may be repeatedly operated between the first control position, the second control position, and the third control position to continue operation of distribution module 450 into next deployment positions.

In various embodiments, adjusting a position of a distribution module in a projectile launcher may comprise translating one or more components of the distribution module. For example, one or more components of the distribution module may be axially translated (e.g., an axial movement). An axial translation may include movement of one or more components of the distribution module in a forward and/or rearward direction. The axial translation may include movement of one or more components of the distribution module from a resting position (e.g., a first position, a first translation position, a rearward position, etc.) to a launch position (e.g., a second position, a second translation position, a forward position, etc.).

In various embodiments, adjusting a position of a distribution module in a projectile launcher may comprise rotating and translating one or more components of the distribution module. In that regard, adjusting a position of a distribution module may include both a circumferential movement and an axial movement. For example, one or more components of the distribution module may be rotated from a first rotational position to a second rotational position and translated from a first translation position to a second translation position. Rotation of the one or more components of the distribution module may occur prior to or together with translation of the one or more components. Translation of the one or more components of the distribution module may occur prior to or together with rotation of the one or more components.

In some embodiments, the one or more components of the distribution module that are rotated may be the same as the one or more components that are translated. For example, a rotating inner housing of the distribution module may be configured to rotate and translate. In some embodiments, at least one of the one or more components of the distribution module that are rotated may be different from at least one of the one or more components that are translated.

In various embodiments, rotation of the one or more components of the distribution module may be caused by a first force and translation of the one or more components of the distribution module may be caused by a second force. The first force may be different from the second force. For example, the first force may be provided mechanically and the second force may be provided fluidly. The first force may be the same as the second force. For example, the first force and the second force may be provided mechanically. In that regard, the first force and the second force may be provided from a same mechanical source or from different mechanical sources.

The first force may be received at a different time from the second force. For example, the first force may be received at a first time and the second force may be received at a second time. The first time may be before the second time. The first time may be approximate to the second time. In some embodiments, the first force may be received at a same time as the second force.

In various embodiments, and with reference to FIGS. 9A-9C, a projectile launcher 900 is disclosed. Projectile launcher 900 may be similar to, or have similar aspects and/or components with, any projectile launcher, CEW, or the like discussed herein. Projectile launcher 900 may comprise a handle 910 and a magazine 912. It should be understood by one skilled in the art that FIG. 9A is a partial schematic representation of projectile launcher 900 depicting components of a propulsion module in a block diagram, and one or more of the components of projectile launcher 900 may be located in any suitable position within, or external to, handle 910. FIGS. 9B and 9C depict projectile launcher 900 with magazine 912 decoupled from handle 910.

In various embodiments, handle 910 may be similar to, or have similar aspects and/or components with, any handle or the like discussed herein. Handle 910 may be configured to house various components of projectile launcher 900 that are configured to enable deployment of projectiles from magazine 912, provide an electrical current to magazine 912, and/or otherwise aid in the operation of projectile launcher 900, as discussed further herein. Handle 910 may comprise various mechanical, electronic, and/or electrical components configured to aid in performing the functions of projectile launcher 900. For example, handle 910 may comprise one or more triggers 915, control interfaces, processing circuits, power supplies, signal generators, and/or the like. Handle 910 may include a guard (e.g., trigger guard). A guard may define an opening formed in handle 910. Trigger 915 may be disposed within a guard.

Handle 910 may comprise a handle end opposite a deployment end. A bay 911 of handle 910 may be configured to receive one or more magazine 912. Bay 911 may comprise an opening in the deployment end sized and shaped to receive one or more magazine 912. Bay 911 may include one or more mechanical features configured to removably couple one or more magazine 912 within bay 911. Handle 910 may comprise one or more interfaces. The one or more interfaces may be disposed within or proximate bay 911. The one or more interfaces may be similar to any other interface (e.g., handle interface) discussed herein, and may comprise a mechanical interface, an electrical interface, an electronic interface, and/or a fluid interface.

In various embodiments, magazine 912 may be similar to, or have similar aspects and/or components with, any magazine or the like discussed herein. Magazine 912 may comprise a housing sized and shaped to be inserted into bay 911. The housing may define one or more bores 953. Each bore 953 may define an opening through the housing (e.g., a chamber). Each bore 953 may be configured to receive a projectile P. Each projectile P may be similar to any other projectile, electrode, or the like disclosed herein. Each bore 953 may be sized and shaped accordingly to receive and house a projectile P prior to and during deployment of the projectile P from magazine 912. Each bore 953 may comprise any suitable deployment angle. One or more bores 953 may comprise similar deployment angles. One or more bores 953 may comprise different deployment angles. The housing may comprise any suitable or desired number of bores 953, such as, for example, two bores, five bores, eight bores (e.g., as depicted), ten bores, and/or the like.

In various embodiments, handle 910 may comprise a propulsion module. The propulsion module may be similar to any other propulsion module disclosed herein. The propulsion module may be in fluid communication with magazine 912, one or more bores 953, and/or one or more projectiles P. The propulsion module may be configured to provide a propulsion force to deploy, or cause deployment of, one or more projectiles P from magazine 912. The propulsion module may comprise any device, propellant, primer, or the like capable of providing a propulsion force. The propulsion force may include an increase in pressure caused by rapidly expanding gas within an area or chamber.

The propulsion module may be configured to receive a propellant from a propulsion source 930 and distribute a propulsion force to one or more projectiles P housed in magazine 912. In response to receiving the propulsion force, the one or more projectiles P may be deployed from magazine 912. Propulsion source 930 may comprise any suitable source of propellant. Propulsion source 930 may be similar to, or share similar components with, any other propulsion source disclosed herein. Propulsion source 930 may be in fluid communication with one or more components of the propulsion module. Propulsion source 930 may be configured to provide a propellant to one or more components of the propulsion module.

In various embodiments, the propulsion module may comprise one or more components configured to receive a propellant, control release of the propellant, distribute the propellant, and/or the like. In that regard, the propulsion module may comprise a valve assembly 927, an activation module 928, and/or a distribution module 950.

In various embodiments, valve assembly 927 may be configured to receive a propellant, store the propellant, and release the propellant. Valve assembly 927 may be similar to any other valve assembly disclosed herein. Valve assembly 927 may be in fluid communication with propulsion source 930 and distribution module 950. Valve assembly 927 may be configured to receive a propellant from propulsion source 930, store the propellant within valve assembly 927, and/or release the propellant to distribution module 950.

In various embodiments, activation module 928 may be configured to control release of a propellant from valve assembly 927. Activation module 928 may be similar to any other activation module, solenoid, and/or the like disclosed herein. Activation module 928 may be configured to engage valve assembly 927 to cause valve assembly 927 to release a propellant. For example, activation module 928 may be configured to mechanically, electrically, electronically, and/or fluidly engage valve assembly 927 to cause valve assembly 927 to release a propellant. Operation of activation module 928 may be controlled by any suitable process, such as, for example, by a processing circuit of handle 910.

In various embodiments, distribution module 950 may be configured to receive a propellant and distribute the propellant. Distribution module 950 may be similar to any other distribution module disclosed herein. Distribution module 950 may be in fluid communication with valve assembly 927 and magazine 912. Distribution module 950 may be configured to receive a propellant from valve assembly 927 and provide a propulsion force to one or more projectiles P housed in magazine 912. In response to receiving the propulsion force, the one or more projectiles P may be launched from magazine 912.

A forward portion of distribution module 950 may extend through (or be accessible from) an inner surface of bay 911 (e.g., as depicted in FIG. 9B). The forward portion of distribution module 950 may align with an end of magazine 912, in response to magazine 912 being coupled within bay 911. In some embodiments, the forward portion of distribution module 950 may contact the end of magazine 912, in response to magazine 912 being coupled within bay 911. In some embodiments, a gap G1 may separate the forward portion of distribution module 950 from the end of magazine 912, in response to magazine 912 being coupled within bay 911 (e.g., as depicted in FIG. 9A).

Distribution module 950 may be configured to selectively provide propulsion force to one or more projectiles P of magazine 912. Selectively providing propulsion force may include adjusting one or more components of distribution module 950 to cause deployment of different projectiles P during discrete deployment events (e.g., discrete trigger activations). Adjusting the one or more components of distribution module 950 may include rotating (e.g., circumferentially) and/or translating (e.g., axially) the one or more components of distribution module 950. Adjustment of distribution module 950 may be controlled mechanically, electrically, electronically, and/or fluidly. For example, rotation of distribution module 950 may be controlled by a processing circuit, operation of trigger 915, and/or the like. Translation of distribution module 950 may be controlled by a processing circuit, a fluid force, a spring force, a recoil force, and/or the like. For example, translation of distribution module 950 from the resting position to the deployment position may be controlled by a fluid force. Translation of distribution module 950 from the deployment position to the resting position may be controlled by a spring force (e.g., a spring coupled to distribution module 950) and/or a recoil force.

In various embodiments, distribution module 950 may comprise a static outer housing 960 and a rotating inner housing. Static outer housing 960 may be similar to any other static outer housing disclosed herein. Static outer housing 960 may comprise one or more static components, structures, and/or the like configured to remain stationary during operation of handle 910 (e.g., static outer housing 960 is not adjusted before, during, or after discrete deployment events). The rotating inner housing may be similar to any other rotating inner housing disclosed herein. The rotating inner housing may comprise one or more adjustable components, structures, and/or the like configured to adjust (e.g., rotate, translate, etc.) during operation of handle 910 (e.g., the rotating inner housing is adjusted before, during, and/or after discrete deployment events). In that regard, in response to distribution module 950 adjusting to selectively provide propellant, the rotating inner housing may rotate and translate while static outer housing 960 remains stationary.

In various embodiments, the rotating inner housing may comprise a cylindrical body 980 and/or a rotational gear (not depicted). Cylindrical body 980 may be similar to any other cylindrical body disclosed herein. Cylindrical body 980 may be disposed (fully or at least partially) within static outer housing 960. Cylindrical body 980 may be configured to rotate and/or translate relative to static outer housing 960. For example, cylindrical body 980 may be configured to rotate within static outer housing 960 and axially translate at least partially out of (e.g., forward) and back into (e.g., rearward) static outer housing 960.

In various embodiments, cylindrical body 980 may define a channel. The channel may be similar to any other channel of a cylindrical body disclosed herein. The channel may be configured to receive and distribute a propulsion force. For example, the channel may define an outlet 985 on a front surface of cylindrical body 980. Outlet 985 may be similar to any other outlet of a cylindrical body disclosed herein. The channel may receive a propulsion force and may distribute the propulsion force at outlet 985. Outlet 985 may be configured to provide a fluid interface to magazine 912, a bore 953, and/or a projectile P. Outlet 985 may be sized and shaped to distribute an amount of propulsion force to cause deployment of the projectile P.

In some embodiments, outlet 985 may comprise a size and shape complimentary to a projectile P. In that regard, outlet 985 may at least partially receive an end of a projectile P during operation of projectile launcher 900. Outlet 985 may provide the amount of propulsion force to the projectile P. Outlet 985 may fluidly seal around the projectile P.

In some embodiments, outlet 985 may comprise a size and shape complimentary to a bore 953 of magazine 912. In that regard, outlet 985 may be configured to align with and/or seal against a bore 953 of magazine 912 during operation of projectile launcher 900. Outlet 985 may provide the amount of propulsion force to the bore 953 of magazine 912. Outlet 985 may fluidly seal around the bore 953 of magazine 912.

In various embodiments, rotation of cylindrical body 980 may change a circumferential position of the channel and outlet 985. For example, rotation of cylindrical body 980 may adjust outlet 985 from a first rotational position to a next rotational position. The next rotational position may be different from the first rotational position. The next rotational position may be circumferentially offset from the first rotational position.

In various embodiments, translation of cylindrical body 980 may change an axial position of the channel and outlet 985. For example, translation of cylindrical body 980 may adjust cylindrical body 980, and the channel and outlet 985, from a first axial position to a next axial position. The next axial position may be different from the first axial position. The next axial position may be forward the first axial position.

The rotational gear may be similar to any other rotational gear, inlet, and/or the like disclosed herein. The rotational gear may be coupled to a rearward surface of cylindrical body 980. The rotational gear may be configured to fluidly couple to a valve assembly and provide a propulsion force from the valve assembly to cylindrical body 980. The rotational gear may be configured to rotate and cause rotation of cylindrical body 980. For example, in response to the rotational gear rotating, cylindrical body 980 may similarly rotate. In that regard, the rotational gear may control rotation of cylindrical body 980. Controlling rotation of cylindrical body 980 may control position of the channel and alignment of outlet 985, which may control selection of one or more projectiles P for deployment.

The rotational gear may comprise one or more structures, components, features, or the like configured to enable rotation of the rotational gear. For example, the rotational gear may comprise one or more axial teeth. The axial teeth may be similar to any other axial teeth of a rotational gear disclosed herein. The rotational gear may comprise one or more structures, components, features, or the like configured to fix the rotational gear into a position during or responsive to a rotation. For example, the rotational gear may comprise one or more radial teeth. The radial teeth may be similar to any other radial teeth of a rotational gear disclosed herein. In some embodiments, the radial teeth may be configured to engage a position tab to fix the rotational gear into a position during or responsive to a rotation.

In various embodiments, the rotating inner housing of a distribution module may be configured to adjust to selectively provide a propulsion force to one or more projectiles of a magazine. The rotating inner housing may adjust by rotating and translating.

For example, the rotating inner housing may rotate from a first rotational position to a next rotational position. Rotation of the rotating inner housing may include rotation of a cylindrical body and a rotational gear of the rotating inner housing. A number of rotational positions may be defined by a number of axial teeth of a rotational gear of the rotating inner housing. In each rotational position the rotating inner housing may be configured to provide a propulsion force to a different set of one or more projectiles. In that regard, rotation of the rotating inner housing may operate to select a set of one or more projectiles for deployment.

As a further example, the rotating inner housing may translate from a resting position (e.g., a first translation position) to a deployment position (e.g., a second translation position). Translation of the rotating inner housing may include translation of the cylindrical body and the rotational gear of the rotating inner housing. Translation of the rotating inner housing may include axial movement of the cylindrical body and the rotational gear in a forward direction or a rearward direction. The rotating inner housing may be configured to translate between two positions. In the resting position, the cylindrical body and be positioned within a static outer housing of the distribution module and a gap (e.g., a gap of air) may exist between the cylindrical body and the magazine. In the deployment position, the rotating inner housing may be translated in a forward direction toward the magazine. The cylindrical body may contact, or be proximate to, the magazine, a bore of the magazine, and/or a projectile loaded into the bore. In the deployment position, the rotating inner housing, including the cylindrical body and the rotational gear, may be closer to the magazine than while in the resting position. In that regard, translation of the rotating inner housing may operate to position the distribution module to provide a propulsion force to cause deployment of a projectile. Positioning the distribution module may include sealing an outlet of the cylindrical body against the projectile or a bore the projectile is loaded into. Sealing the outlet may at least partially reduce a loss of propulsion force provided to the projectile. Scaling the outlet may at least partially increase a velocity the projectile is deployed at.

In various embodiments, the rotating inner housing may be configured to rotate and translate in any order. For example, the rotating inner housing may be configured to first rotate into a next position to select a set of one or more projectiles to be deployed. The rotating inner housing may then be configured to translate into the deployment position before providing a propulsion force to cause deployment of the set of one or more projectiles.

In various embodiments, and with reference to FIGS. 10A and 10B, distribution module 950 is depicted translating from a resting position to a deployment position.

Distribution module 950 may be positioned proximate magazine 912 with gap G1 (e.g.,

a first gap) separating cylindrical body 980 from magazine 912. Cylindrical body 980 may be positioned within static outer housing 960. A rotational gear 990 may be coupled to cylindrical body 980. The coupling between rotational gear 990 and cylindrical body 980 may include one or more O-rings configured to at least partially reduce a loss of fluid transmitted between rotational gear 990 and cylindrical body 980. For example, rotational gear 990 may comprise one or more circumferential channels. An O-ring may be positioned within the one or more circumferential channels. The O-ring may at least partially seal against a surface of cylindrical body 980.

Rotational gear 990 may be separated from static outer housing 960 by a gap G2 (e.g., a second gap). Gap G2 may be similar to gap G1. Gap G2 may comprise a similar distance (e.g., measured between surfaces defining the respective gap) as gap G1. In some embodiments, gap G2 may comprise a same distance as gap G1.

Distribution module 950 may be fluidly coupled to valve assembly 927. For example, an outlet 999 (e.g., a valve assembly outlet) of valve assembly 927 may be fluidly coupled to an opening 993 (e.g., a rotational gear opening) of rotational gear 990. A channel 987 of cylindrical body 980 may be fluidly coupled to opening 993. Channel 987 may be in fluid communication with outlet 985. In that regard, a propulsion source may be provided by valve assembly 927, through rotational gear 990, and through channel 987 to outlet 985.

In various embodiments, rotational gear 990 may comprise an inlet 998 (e.g., a rotational gear inlet). Inlet 998 may be similar to any other inlet of a distribution module disclosed herein. Inlet 998 may comprise an axial protrusion extending towards valve assembly 927. Inlet 998 may define opening 993. Inlet 998 may be configured to surround outlet 999 of valve assembly 927. Inlet 998 may be configured to slidably couple to outlet 999 of valve assembly 927. The coupling between inlet 998 and outlet 999 may include one or more O-rings configured to at least partially reduce a loss of fluid transmitted between valve assembly 927 and distribution module 950. For example, valve assembly 927 may comprise one or more circumferential channels. An O-ring may be positioned within the one or more circumferential channels. The O-ring may at least partially seal against an inner surface of inlet 998 of rotational gear 990.

In various embodiments, a surface area of outlet 999 may be greater than a surface area of opening 993. For example, outlet 999 may define a first surface area and opening 993 may define a second surface area. The first surface area may be greater than the second surface area.

In various embodiments, as valve assembly 927 provides a propulsion force via outlet 999 a fluid pressure may build against the surface of rotational gear 990 due to the first surface area of outlet 999 being greater than the second surface area of opening 993. For example, a first portion of the propulsion force provided by valve assembly 927 may enter through outlet 999 while a second portion of the propulsion force applies pressure against the surface of rotational gear 990. The fluid pressure may cause rotational gear 990 and cylindrical body 980 to translate in an axially forward direction. In that regard, the fluid pressure caused by provision of a propulsion force from valve assembly 927 may cause rotational gear 990 and cylindrical body 980 to translate from a resting position to a deployment position. Translation of rotational gear 990 may cause rotational gear 990 to enter gap G2. Translation of rotational gear 990 may cause rotational gear 990 to contact static outer housing 960. Translation of cylindrical body 980 may cause cylindrical body 980 to enter gap G1. Translation of cylindrical body 980 may cause cylindrical body 980 to contact magazine 912. Contact of magazine 912 may comprise outlet 985 contacting or aligning with a bore 953 and/or a projectile P.

In various embodiments, contact of cylindrical body 980 against magazine 912 (and/or against a bore 953 and/or a projectile P) may impart a recoil force (e.g., a rearward force) against cylindrical body 980. The recoil force may cause cylindrical body 980 and rotational gear 990 to translate in an axially rearward direction. In that regard, the recoil force may cause cylindrical body 980 and rotational gear 990 to translate from the deployment position back into the resting position.

In various embodiments, the propulsion force may be provided from outlet 985 to launch a projectile P from magazine 912 prior to, or together with, the recoil force being imparted on cylindrical body 980. In that regard, the propulsion force may be provided from outlet 985 while cylindrical body 980 and rotational gear 990 are in the deployment position. The projectile P may be launched from magazine 912 while cylindrical body 980 and rotational gear 990 are in the deployment position. After or during launch of the projectile P, the recoil force may be imparted on cylindrical body 980 to cause cylindrical body 980 and rotational gear 990 to return to the resting position.

In various embodiments, and with specific reference to FIG. 10A, distribution module 950 is depicted in the resting position. Cylindrical body 980 is separated from magazine 912 by gap G1. Rotational gear 990 is separated from static outer housing 960 by a gap G2. In response to a rotation of cylindrical body 980 and rotational gear 990, channel 987 and outlet 985 may be aligned to provide a propulsion force to a bore 953 and/or a projectile P housed in magazine 912.

In response to an activation event of a projectile launcher, valve assembly 927 may provide a propulsion force to distribution module 950. As the propulsion force is provided from outlet 999 of valve assembly 927 into opening 993 of rotational gear 990, a pressure force may build against a surface of rotational gear 990 causing rotational gear 990 and cylindrical body 980 to translate in an axially forward direction. Translation in the axially forward direction may cause rotational gear 990 and cylindrical body 980 to translate from the resting position to the deployment position.

In various embodiments, and with specific reference to FIG. 10B, distribution module 950 is depicted in the deployment position. Translation of rotational gear 990 and cylindrical body 980 may cause cylindrical body 980 to enter gap G1. Cylindrical body 980 may contact magazine 912. Outlet 985 of cylindrical body 980 may contact bore 953 and/or projectile P. Contact of bore 953 and/or projectile P may include outlet 985 sealing against one of bore 953 and/or projectile P. In some embodiments, sealing against one of bore 953 and/or projectile P may include at least a portion of projectile P being inserted into outlet 985. Translation of rotational gear 990 and cylindrical body 980 may cause rotational gear 990 to enter gap G2. Rotational gear 990 may contact static outer housing 960. Inlet 998 of rotational gear 990 may slide axially forward while maintaining fluid coupling between valve assembly 927 and distribution module 950. Outlet 999 of valve assembly 927 may be separated from opening 993 of rotational gear 990 while maintaining fluid coupling between valve assembly 927 and distribution module 950.

The propulsion force may be provided through channel 987 and outlet 985 to projectile P. In response to receiving the propulsion force, projectile P may be launched from magazine 912.

In various embodiments, launch of projectile P and/or impact of cylindrical body 980 against magazine 912 may impart a recoil force to cylindrical body 980. The recoil force may cause cylindrical body 980 and rotational gear 990 to move in an axially rearward direction. The axially rearward movement may cause cylindrical body 980 and rotational gear 990 to translate from the deployment position back to the resting position.

In various embodiments, subsequent activation events of the projectile launch may cause distribution module 950 to continue to rotate between different rotational positions and translate between the resting position and the deployment position.

In various embodiments, and with reference to FIG. 11, a method 1101 for deploying a projectile using a distribution module of a propulsion module is disclosed. Method 1101 may be performed by any suitable device, system, launcher, and/or the like. Different steps of method 1101 may be performed by the same device, system, launcher, and/or the like. Different steps of method 1101 may be performed by one or more different devices, systems, launchers, and/or the like. In some embodiments, method 1101 may be performed by a projectile launcher.

A projectile launcher may receive a trigger activation (step 1102). For example, the trigger of the projectile launcher may be activated (e.g., depressed, pulled, etc.). The trigger activation may comprise a mechanical activation, an electrical activation, an electronic activation, or the like. A processing circuit of the projectile launcher may detect, or receive data indicating, the trigger activation.

A projectile launcher may adjust a distribution module of a propulsion module (step 1104). The distribution module may be adjusted based on the trigger activation. Adjusting the distribution module may comprise rotating a rotating cylinder of the distribution module to align an outlet with a first set of projectiles (including one or more projectiles). The distribution module may be rotated into one or more deployment positions (e.g., a first deployment position, a second deployment position, etc.). For example, during a first activation the distribution module may be rotated into a first deployment position. In some embodiments, the distribution module may be rotated based on instructions from or control by the processing circuit. In some embodiments, the distribution module may be mechanically coupled to the trigger via a control assembly. The trigger activation may mechanically translate the control assembly to cause rotation of the distribution module.

A projectile launcher may activate a valve assembly of the propulsion module (step 1106). The valve assembly may be activated based on the trigger activation. The valve assembly may control provision of a fluid source (e.g., a propellant). The valve assembly may be in fluid communication with the distribution module. Activating the valve assembly may cause the valve assembly to provide an amount of the fluid to the distribution module. In some embodiments, the valve assembly may be activated by the processing circuit. In some embodiments, the valve assembly may be activated by an activation module of the propulsion module. In some embodiments, the valve assembly may be activated based on adjusting the distribution module in step 1104.

In various embodiments, activation of the valve assembly may cause the distribution module to adjust. For example, the amount of fluid provided to the distribution module may cause the distribution module to translate from a resting position to a deployment position. A cylindrical body and a rotational gear of the distribution module may translate while a static outer housing of the distribution module remains in position. Translation to the deployment position may align the distribution module with a bore and/or a projectile of a magazine.

In various embodiments, step 1104 may be performed prior to step 1106. In various embodiments, step 1106 may be performed prior to step 1104. In various embodiments, step 1104 may be performed simultaneously with, or in close proximity of time to, step 1106.

A projectile launcher may deploy a projectile (step 1108). The projectile may be aligned, or in fluid communication, with the outlet of the distribution module adjusted into a deployment position in step 1104 and/or step 1106. The projectile may be deployed based on the amount of fluid provided in step 1106. For example, propellant released by the valve assembly may travel through the distribution module and via the outlet. Responsive to receiving the propellant, the projectile may be deployed from the projectile launcher.

In various embodiments, in response to the projectile launcher comprising a CEW, the projectile launcher may provide a stimulus signal through the launched projectile.

In various embodiments, responsive to deployment of the projectile, the distribution module may return from the deployment position back to the resting position.

A projectile launcher may receive a next trigger activation (step 1110). In response to receiving the next trigger activation, the projectile launcher may repeat steps 1104, 1106, and 1108. For example, the projectile launcher may adjust the distribution module into a next position. The projectile launcher may activate the valve assembly to release an amount of fluid. The distribution module may adjust from the resting position to the deployment position. The amount of fluid may travel through the distribution module to deploy a next projectile.

In various embodiments, a propulsion module for a projectile launcher is disclosed. The propulsion module may comprise a valve assembly and a distribution module. The distribution module may be in fluid communication with the valve assembly. The distribution module may be configured to adjust to selectively provide a propellant to one or more projectiles. The distribution module may be configured to adjust by a physical movement of the distribution module from a first position to a second position.

In various embodiments of the above propulsion module, the physical movement may comprise a rotational movement. The second position may be circumferentially offset from the first position. The physical movement may comprise an axial translation. The second position may be axially offset from the first position. The physical movement may comprise a rotational movement and an axial translation. The first position may comprise a first rotational position and a first translation position, the second position may comprise a second rotational position and a second translation position, the second rotational position may be circumferentially offset from the first rotational position, and the second translation position may be axially offset from the first translation position. The rotational movement may occur before the axial translation. The rotational movement may occur at least one of before or during the axial translation. The distribution module may comprise a static outer housing and a rotating inner housing. The static outer housing may remain stationary during the physical movement, and the rotating inner housing may adjust during the physical movement.

In various embodiments, a handle for a projectile launcher is disclosed. The handle may comprise a body defining a bay and a propulsion module disposed within the body proximate the bay. The propulsion module may comprise a distribution module configured to adjust to selectively provide a propellant to one or more projectiles. The distribution module may be configured to adjust by a physical movement of the distribution module from a first position to a second position.

In various embodiments of the above handle, in the first position the distribution module may be configured to provide the propellant to a first group of projectiles from the one or more projectiles, and in the second position the distribution module may be configured to provide the propellant to a second group of projectiles from the one or more projectiles. The distribution module may be configured to rotate from the first position to the second position. The distribution module may comprise an outlet, and responsive to rotation of the distribution module the outlet may be configured to align with a different group of projectiles from the one or more projectiles. In the first position the distribution module may be separated from the one or more projectiles by a gap, and in the second position the distribution module may be proximate the one or more projectiles. The distribution module may be configured to translate from the first position to the second position. The distribution module may comprise an outlet, and responsive to translation of the distribution module the outlet may be configured to seal against a projectile from the one or more projectiles.

In various embodiments, a method of deploying a projectile from a projectile launcher is disclosed. The method may comprise the steps of receiving a trigger activation; rotating a distribution module of a propulsion module, wherein in response to the rotating an outlet of the distribution module is aligned with the projectile; activating a valve assembly of the propulsion module, wherein in response to the activating the valve assembly provides a propellant to the distribution module; and translating the distribution module in an axially forward direction towards the projectile, wherein the distribution module provides the propellant to the projectile to cause deployment of the projectile.

In various embodiments of the above method, the rotating may be in response to the trigger activation, and the translating may be in response to the valve assembly providing the propellant to the distribution module.

In various embodiments, a propulsion module for a projectile launcher is disclosed. The propulsion module may comprise a valve assembly and a distribution module in fluid communication with the valve assembly. The distribution module may be configured to rotate into a plurality of deployment positions.

In various embodiments of the above propulsion module, the distribution module may be configured to receive a propellant from the valve assembly, the distribution module may be configured to provide the propellant to a first projectile in response to the distribution module being rotated into a first deployment position of the plurality of deployment positions, and the distribution module may be configured to provide the propellant to a next projectile in response to the distribution module being rotated into a next deployment position of the plurality of deployment positions. Each deployment position of the plurality of deployment positions may be configured to allow deployment of a different projectile. The distribution module may be configured to receive a mechanical force to cause the distribution module to rotate into the plurality of deployment positions. The distribution module may comprise a stationary structure and a rotating structure, and the rotating structure may be configured to rotate within the stationary structure. The stationary structure and the rotating structure may share a common axis. The distribution module may further comprise an activation module configured to control release of a propellant from the valve assembly. The activation module may be configured to control release of the propellant from the valve assembly after rotation of the distribution module into a deployment position of the plurality of deployment positions. The activation module may be configured to control release of the propellant from the valve assembly during rotation of the distribution module into a deployment position of the plurality of deployment positions.

In various embodiments, a projectile launcher is disclosed. The projectile launcher may comprise a handle defining a bay and a propulsion module disposed within the handle proximate the bay. The propulsion module may comprise a distribution module configured to rotate into a plurality of deployment positions.

In various embodiments of the above projectile launcher, the projectile launcher may further comprise a magazine removably coupled within the bay of the handle, and the magazine may comprise a plurality of projectiles. Each deployment position of the plurality of deployment positions may be configured to allow deployment of a different projectile of the plurality of projectiles. The distribution module may comprise an outlet, and responsive to rotation of the distribution module the outlet may be aligned with a different projectile of the plurality of projectiles. The distribution module may extend from within the handle into the bay of the handle. The distribution module may comprise a stationary structure and a rotating structure, and the rotating structure may be configured to rotate within the stationary structure. The stationary structure may be coupled to an inner surface of the handle.

In various embodiments, a method of deploying a projectile from a projectile launcher is disclosed. The method may comprise one or more steps including: receiving a trigger activation; rotating a distribution module of a propulsion module based on the trigger activation, wherein in response to the rotating the distribution module is aligned with the projectile in a first deployment position; and activating a valve assembly of the propulsion module, wherein in response to the activating the valve assembly provides a propellant to the distribution module causing deployment of the projectile.

In various embodiments of the above method, the one or more steps may further comprise: receiving a next trigger activation; next rotating the distribution module based on the next trigger activation, wherein in response to the next rotating the distribution module is aligned with a next projectile in a next deployment position; and next activating the valve assembly, wherein in response to the next activating the valve assembly provides the propellant to the distribution module causing deployment of the next projectile. The trigger activation may apply a mechanical force to the distribution module, and the mechanical force may cause the distribution module to rotate. The rotating may be performed before the activating.

In various embodiments, a propulsion module for a projectile launcher is disclosed. The propulsion module may comprise a valve assembly and a distribution module in fluid communication with the valve assembly. The distribution module may be configured to translate between a resting position and a deployment position. The deployment position may be axially forward the resting position.

In various embodiments of the above propulsion module, the valve assembly may be configured to provide a propellant to the distribution module, and the distribution module may be configured to provide the propellant to a first projectile in response to the distribution module being translated into the deployment position. The distribution module may be configured to translate from the resting position to the deployment position in response to the valve assembly providing the propellant to the distribution module. The first projectile may be configured to deploy in response to receiving the propellant from the distribution module, and the distribution module may be configured to translate from the deployment position to the resting position in response to the first projectile deploying. The first projectile deploying may impart a recoil force on the distribution module, and the recoil force may be configured to translate the distribution module from the deployment position to the resting position. The distribution module may be configured to receive a fluid force to cause the distribution module to translate from the resting position to the deployment position. The distribution module may be configured to receive a spring force to cause the distribution module to translate from the resting position to the deployment position. The distribution module may comprise a stationary structure and a rotating structure, and the rotating structure may be configured to translate within or forward of the stationary structure. The stationary structure and the rotating structure may share a common axis.

In various embodiments, a projectile launcher is disclosed. The projectile launcher may comprise a handle and a magazine removably coupled within a bay of the handle. The handle may comprise a body defining the bay and a propulsion module disposed within the body proximate the bay. The propulsion module may comprise a distribution module configured to translate between a resting position and a deployment position. The deployment position may be axially forward the resting position, The magazine may comprise a plurality of bores defined through the magazine and a plurality of projectiles, and each projectile of the plurality of projectiles may be configured be disposed into a bore of the plurality of bores.

In various embodiments of the above projectile launcher, the distribution module may be configured to at least partially extend into the bay. In response to the magazine being coupled within the bay, the distribution module may be separated from the magazine by a gap while in the resting position. In response to the distribution module translating into the deployment position, the distribution module may be configured to move forward into the gap. The distribution module may be closer to the magazine in the deployment position than in the resting position. In the deployment position the distribution module may be configured to contact at least one of the magazine, a bore of the plurality of bores, or a projectile of the plurality of projectiles. In the deployment position the distribution module may be configured to seal against at least one of a bore of the plurality of bores or a projectile of the plurality of projectiles. In the deployment position an end of a projectile of the plurality of projectiles may be received within the distribution module.

In various embodiments, a method of deploying a projectile from a projectile launcher is disclosed. The method may comprise one or more steps including: receiving a trigger activation; activating a valve assembly of a propulsion module of the projectile launcher, wherein in response to the activating the valve assembly provides a propellant to a distribution module of the propulsion module; and forward translating the distribution module to a deployment position towards the projectile, wherein the distribution module provides the propellant to the projectile to cause deployment of the projectile.

In various embodiments of the above method, the forward translating may be in response to the valve assembly providing the propellant to the distribution module. The one or more steps may further comprise: rearward translating the distribution module to a resting position; receiving a next trigger activation; next activating the valve assembly, wherein in response to the next activating the valve assembly provides a next propellant to the distribution module; and next forward translating the distribution module to the deployment position towards a next projectile, wherein the distribution module provides the next propellant to the next projectile to cause deployment of the next projectile. The rearward translating may be in response to a first force provided to the distribution module, the next forward translating may be in response to a second force provided to the distribution module, and the first force may be different from the second force.

In various embodiments, a distribution module for a propulsion module of a projectile launcher is disclosed. The distribution module may comprise a static outer housing, a cylindrical body, and a rotational gear. The static outer housing may comprise a first static outer housing end opposite a second static outer housing end. The first static outer housing end may define a static outer housing opening. The cylindrical body may be disposed within the static outer housing opening. The cylindrical body may comprise a first cylindrical body end opposite a second cylindrical body end. The rotational gear may be coupled to the second cylindrical body end. The cylindrical body and the rotational gear may be configured to physically move while the static outer housing remains stationary.

In various embodiments of the above distribution module, the static outer housing, the cylindrical body, and the rotational gear may share a common axis. The cylindrical body may be configured to rotate within the static outer housing. The rotational gear may be configured to receive a force to cause the rotational gear and the cylindrical body to rotate. The rotational gear may comprise a plurality of axial teeth extending rearward from the rotational gear. The plurality of axial teeth may be configured to receive the force to cause the rotational gear and the cylindrical body to rotate. The cylindrical body may be configured to rotate into a plurality of deployment positions. The rotational gear may be configured to position the cylindrical body into each deployment position of the plurality of deployment positions. The rotational gear may comprise a plurality of radial teeth extending radially outward from the rotational gear, and the plurality of radial teeth may be configured to position the cylindrical body into each deployment position of the plurality of deployment positions. The distribution module may further comprise a position tab coupled to the static outer housing proximate the second static outer housing end, and the position tab may be configured to engage a radial tooth of the plurality of radial teeth to position the cylindrical body into a deployment position of the plurality of deployment positions. The cylindrical body may be configured to translate in an axially forward direction away from the static outer housing or an axially rearward direction toward the static outer housing. The cylindrical body may be configured to translate from a resting position to a deployment position, in the resting position the first cylindrical body end may be proximate the first static outer housing end, and in the deployment position the first cylindrical body end may be axially forward the first static outer housing end. The second static outer housing end may be at least partially positioned between the rotational gear and the cylindrical body. The rotational gear may be separated from the second static outer housing end by a gap. In response to the cylindrical body translating in the axially forward direction, the rotational gear may translate axially forward into the gap. In response to the cylindrical body translating in the axially forward direction, the rotational gear may contact the second static outer housing end. The rotational gear may be fluidly coupled to the cylindrical body. The cylindrical body may comprise a channel defined through the cylindrical body from the second cylindrical body end to the first cylindrical body end, the cylindrical body may comprise an outlet defined on the first cylindrical body end, and the outlet may be in fluid communication with the channel. The rotational gear may comprise an inlet defining an opening configured to receive a propellant, and the opening may be in fluid communication with the channel. The opening may be configured to receive the propellant from a valve assembly outlet of a valve assembly, and the inlet may be configured to at least partially seal against the valve assembly outlet. The valve assembly outlet may comprise a first surface area, the opening may comprise a second surface area, and the first surface area may be greater than the second surface area.

Benefits, other advantages, and solutions to problems have been described herein with regard to specific embodiments. Furthermore, the connecting lines shown in the various figures contained herein are intended to represent exemplary functional relationships and/or physical couplings between the various elements. It should be noted that many alternative or additional functional relationships or physical connections may be present in a practical system. However, the benefits, advantages, solutions to problems, and any elements that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as critical, required, or essential features or elements of the disclosures. The scope of the disclosure is accordingly to be limited by nothing other than the appended claims and their legal equivalents, in which reference to an element in the singular is not intended to mean “one and only one” unless explicitly so stated, but rather “one or more.” Moreover, where a phrase similar to “at least one of A, B, or C” is used in the claims, it is intended that the phrase be interpreted to mean that A alone may be present in an embodiment, B alone may be present in an embodiment, C alone may be present in an embodiment, or that any combination of the elements A, B, and C may be present in a single embodiment; for example, A and B, A and C, B and C, or A and B and C.

Systems, methods, and apparatus are provided herein. In the detailed description herein, references to “various embodiments,” “some embodiments,” “one embodiment,” “an embodiment,” “an example embodiment,” etc., indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Further, when a particular feature, structure, or characteristic is described in connection with an embodiment, it is submitted that it is within the knowledge of one skilled in the art to affect such feature, structure, or characteristic in connection with other embodiments whether or not explicitly described. After reading the description, it will be apparent to one skilled in the relevant art(s) how to implement the disclosure in alternative embodiments. Furthermore, no element, component, or method step in the present disclosure is intended to be dedicated to the public regardless of whether the element, component, or method step is explicitly recited in the claims. No claim element is intended to invoke 35 U.S.C. 112(f) unless the element is expressly recited using the phrase “means for.” As used herein, the terms “comprises,” “comprising,” or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.