Single stage to orbit rocket engine

EVANESCENT OR FUGACIOUS THRUST DEFLECTOR

Steering system with power take-off from actuators

ROCKET BRAKED BY AIR RECOVERED BY TURBINES AND DECELERATION METHOD FOR RECOVERY OF SAME

Liquid propellant rocket engine nozzle with passive condensate cooling

Vehicle attitude control using movable mass

Aerospike rocket motor assembly

THRUST VECTORING DEVICE

Vehicle attitude control using jet paddles and/or movable mass

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

Electrically powered propulsion system for use in a spacecraft

Thrust vectoring apparatus, thrust vectoring method, and flying body

System for steering, about its axes of rotation, a moving body propelled by jet reaction, particularly a missile

System for controlling the trajectory of a jet-propelled mobile

Flying object

Spacecraft afterbody device

Jet vane and method for manufacturing a jet vane

Component for use in streams of hot gas

Integral thrust vector and roll control system

FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE

Nozzle assembly for rocket and ramjet applications

Thrust augmentation in plug nozzles and expansion-deflection nozzles

Asonic aerospike engine

Method for reducing jet tab exposure during thrust vectoring