HEAT SHIELD WITH RECESSED DUAL-EXPANSION NOZZLE, AND VEHICLE INCLUDING THE SAME

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

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTON

EXHAUST NOZZLE

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

ROCKET INJECTOR SUBSCALE STABILITY ASSESSMENT WITH TELESCOPING PISTON

Rocket propulsion systems and associated methods

THRUSTER NOZZLE ASSEMBLY WITH FLOW REGULATOR IN THROAT AREA AND ROTARY JOINT

Rocket propulsion systems and associated methods

Attitude control and thrust boosting system and method for space launchers

BOOST THRUST ROCKET MOTOR

POWER MODULES FOR HYPERSONIC VEHICLES

Resin transfer molded rocket motor nozzle with adaptive geometry

Thrust control apparatus of propulsion system

Thruster control device and thruster control method

Device for modulating a gas ejection section

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

Electrically operated propellant for solid rocket motor thrust management

Device for modulating a gas ejection section

Solid propellant rocket motor

Pulse detonation drive

Thrust control valve and flying object

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

Device for modulating a gas ejection section

Nozzle having a variable neck section for a spacecraft thruster provided with a mobile needle

Orbit attitude control device, and method of controlling orbit attitude

Engine for use in an aerial vehicle

Rocket multi-nozzle grid assembly and methods for maintaining pressure and thrust profiles with the same

Propulsion system with movable thermal choke

Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle

Variable slope exhaust nozzle

Pintle-controlled propulsion system with external ring actuator

Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles

Nozzle with temperature-responsive throat diameter

Pintle-controlled propulsion system with external dynamic seal

Nozzles with rotatable sections for variable thrust

Missile control system and method

Method of manufacturing a duct for a gas turbine engine

Thrust vector control system for a plug nozzle rocket engine

System for multiple burns from a rocket motor

Thrust control apparatus having inner and outer pintle nozzles controlled by common gear