Nozzle with Widely-Spaced Thrust Chambers, Engine Including the Nozzle, and Vehicle Including the Engine

High Temperature Thermal Protection System for Rockets, and Associated Methods

Augmented Aerospike Nozzle, Engine Including the Augmented Aerospike Nozzle, and Vehicle Including the Engine

ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED HEAT SHIELD

SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS

REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING THROAT OR MOVEABLE INJECTOR PLATE

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTON

Whispering gallery mode fusion power plant and rocket propulsion

ROCKET ENGINE WITH DUAL CONTOUR NOZZLE

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE

SCALEABLE ACOUSTICALLY-STABLE COMBUSTION CHAMBER AND DESIGN METHODS

REUSABLE UPPER STAGE ROCKET

Dynamic quick connector coupling

Single stage to orbit rocket engine

Transpiration-cooled systems having permeable and non-permeable portions

Transpiration-cooled systems having permeable and non-permeable portions

Bobbin-Form Solid Controlled and Filament Fed Hybrid Propulsion Methods for Space Vehicle Innovative Architectures

Zero emission supersonic fan engine

Rocket engine with dual contour nozzle

Duplex Turbine Guide Vane Assembly

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING THROAT OR MOVEABLE INJECTOR PLATE

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTON

Non-axisymmetric heat shield, a nozzle defined at least partially by the heat shield, an engine including the nozzle, and a vehicle including the engine

Annular aerospike nozzle with widely-spaced thrust chambers, engine including the annular aerospike nozzle, and vehicle including the engine

ADDITIVELY MANUFACTURED, THERMALLY OPTIMIZED ROCKET MOTOR NOZZLE DESIGN

Duplex Turbine Guide Vane Assembly

Rocket engine with dual contour nozzle

Augmented aerospike nozzle, engine including the augmented aerospike nozzle, and vehicle including the engine

ADDITIVELY MANUFACTURED BELLOWS

AEROSPIKE ENGINES, LAUNCH VEHICLES INCORPORATING SUCH ENGINES AND METHODS

JET NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME

Laser assisted steam energized rocket (L.A.S.E.R.)

Reusable upper stage rocket with aerospike engine

Structure for assembling a piece comprising a first metal part and a second part made of an organic matrix composite material

STRUCTURE FOR ASSEMBLING A PIECE COMPRISING A FIRST METAL PART AND A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL

METAL-ORGANIC FRAMEWORK MATERIAL-BASED FUELS AND METHODS OF USE THEREOF

Catalyst System for Rocket Engine

Combustor of liquid rocket engine

Multi-mode combined cycle propulsion engine

HYDROGEN EJECTOR FOR ROCKET ENGINE

Thermal protection device for a nozzle

Hybrid propulsion unit for space vehicle

SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS

Ring-shaped booster rocket

Ring-shaped booster rocket

Jet nozzle equipped with a thermally regulated ring

High temperature thermal protection system for rockets, and associated methods

Thrust Augmentation for Liquid Rocket Engines

Distributed airfoil aerospike rocket nozzle

SCREW ROCKET NOZZLE

Upper stage rocket including aerospike nozzle defining actively-cooled re-entry heat shield

Hybrid metal composite structures, rocket motors including hybrid metal composite structures, and related methods

Multi-pulse gas generator device and igniter with varied flow rates

Hybrid metal composite structures, joint structures, and related methods

Liquid rocket engine assemblies and related methods

DYNAMIC ROCKET NOZZLE

System for controlling speed transition and thrust vectorisation in a multiple-shaped nozzle by secondary injection

Attitude control and thrust boosting system and method for space launchers

BOOST THRUST ROCKET MOTOR

Composite material fabrication method

Scaleable acoustically-stable combustion chamber and design methods

AEROSPIKE/BELL HYBRID ROCKET ENGINE WITH COMBINED BELL NOZZLE WITHIN AN AEROSPIKE NOZZLE

METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART PROVIDED WITH A SENSOR

Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites

Thrust control apparatus of propulsion system

Hybrid metal composite structures, joint structures, and related methods

SCREW ROCKET NOZZLE

NUCLEAR THERMAL PROPULSION ROCKET ENGINE

System for assembly and disassembly of a rocket motor

Rocket motor with composite divergent nozzle section

Rocket engine including a lashing device

Resin transfer molded rocket motor nozzle

Liquid propellant rocket engine nozzle with passive condensate cooling

ROCKET ENGINE COMBUSTION CHAMBER LINER

Ceramic matrix composite component and method of producing the same

TRREN exhaust nozzle-M-spike turbo ram rocket

Composite material based on C/SiC fibers with ultra refractory, high tenacity and ablation resistant matrix

Hybrid Rocket Motor

Fragmenting nozzle system

Induction ignition device for initiating a fuel burn

ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AIRPLANE TAKEOFF, LANDING OR IN-FLIGHT MANEUVERABILITY

Solid rocket propellant with low glass transition

Assembly including aft end igniter for rocket motor

HYBRID METAL COMPOSITE STRUCTURES, ROCKET MOTORS AND MULTI-STAGE ROCKET MOTOR ASSEMBLIES INCLUDING HYBRID METAL COMPOSITE STRUCTURES, AND RELATED METHODS

MICROPUMP-FED AUTOGENOUS PRESSURIZATION SYSTEM

SOLID ROCKET MOTOR WITH BARRIER

Liquid rocket engine assemblies and related methods

Dual stage catalytic thruster

Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings

Electrically operated propellant for solid rocket motor thrust management

Anti-stall hydraulic pump for a thrust vector control system

Scalable acoustically-stable combustion chamber and design methods

Integrated thruster

Projectile with single-piece main body

Rocket apparatuses, systems and methods

Hybrid metal composite structures, rocket motors and multi stage rocket motor assemblies including hybrid metal composite structures, and related methods

Rocket thruster nozzle with connectors and brace

Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites

Passive reactivity control of nuclear thermal propulsion reactors

Rocket engine bipropellant supply system including an electrolyzer

Persistent vortex generating high regression rate solid fuel grain for a hybrid rocket engine and method for manufacturing same

Method for creating engine thrust

Aerospike rocket motor assembly

Thrust nozzle with double contour and smooth transition

Engine for a spacecraft, and spacecraft comprising such an engine

Pulse detonation drive

Rotating pulse detonation engine, power generation system including the same, and methods of making and using the same

Ductile high-temperature molybdenum-based alloys

VAPOR JET SYSTEM

Fragmenting nozzle system

Pneumatic circuit breaker based self resetting passive overspeed control valve for turbine pump assembly

PASSIVE ELECTRICAL PROPORTIONAL TURBINE SPEED CONTROL SYSTEM

Spring-assisted deployment of a pivotable rocket motor

Rocket motor propellants, systems and/or methods

Propulsion unit for reusable launch vehicle

Vehicle attitude control using jet paddles and/or movable mass

Low-thickness thermostructural composite material part, and manufacture method

Combustion gas discharge nozzle for a rocket engine provided with a sealing device between a stationary part and a moving part of the nozzle

Deflector for a thrust flow powered vehicle and thrust flow powered vehicle with said deflector

Reduction of rocket jet stream dispersion

Stable hybrid rocket technology

Nozzle having a movable divergent section with a thermal protection system

Rocket motors and their use

Method and apparatus for variable exhaust nozzle exit area

Propellant with extended storage life

RESIN TRANSFER MOLDED ROCKET MOTOR NOZZLE

NOZZLE ARRANGEMENT FOR AN ENGINE

ENGINE PROPULSION SYSTEM

ROTARY PULSE DETONATION ENGINE

Gas turbine engine nozzle including housing having scalloped root regions

Threaded rod for system for deploying a deployable divergent segment of a thruster

Slotted multi-nozzle grid with integrated cooling channels

Thruster and spacecraft

Engine apparatus and method for reducing a side load on a flying object

Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold

Combustion chamber provided with a tubular element

Fluid injection system

Vortex cannon with enhanced ring vortex generation

SYSTEM AND METHOD FOR CONTROLLING AN OBJECT TRAVELING THROUGH EXOATMOSPHERIC SPACE

Hybrid exhaust component

Low-thickness thermostructural composite material part, and manufacture method

Space debris removal

Belted toroid pressure vessel and method for making the same

Combustion chamber comprising a condensation-proof barrier on a regenerative circuit

SUPERSONIC COMBUSTOR ROCKET NOZZLE

Method of producing a nozzle or a divergent nozzle element made of a composite

Propulsion system with canted multinozzle grid

Propulsion system and method using a combustion chamber discharging a concentrated mass

Fastener assembly for connecting rocket engine nozzles

Device for damping the lateral forces due to jet separation acting on a rocket engine nozzle

Pintle-controlled propulsion system with external ring actuator

Nozzle with temperature-responsive throat diameter

Rocket engine nozzle system

Method of fabricating a rocket engine nozzle using pressure brazing

Method of producing a fibrous layer for the manufacture of a preform of a composite part

Integral composite rocket motor dome/nozzle structure

Exhaust assembly for missile system, and method

Heat shield for mounting on a heat-radiating object, particularly on a rocket engine

Outlet nozzle and a method for manufacturing an outlet nozzle

Acoustic dampers

Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing

Multilayer composite

Lightweight rocket engine combustion chamber and associated method

Phenolic lamination process for hot gas components

Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine

Asonic aerospike engine

Boost injection turbine exhaust cycle (BITEC)

Thin-walled high temperature alloy structures via multi-material additive manufacturing

Thin-walled high temperature alloy structures via multi-material additive manufacturing

Thrust chamber liner and fabrication method therefor

Liquid monopropellant controlled solid rocket motor with aft end injection deflector

Seal for gimbaling and/or fixed rocket engine nozzles, and associated systems and methods

Multi-pulse rocket propulsion motor

Monofilament vaporization propulsion systems

Electrothermal space thruster heater for decomposable propellants

Nozzled mortar ignition system for improved performance