ROCKET ENGINE WITH DUAL CONTOUR NOZZLE

THRUST VECTOR CONTROL FOR HYBRID PROPELLANTS ROCKET ENGINE WITH EMBEDDED FLUID INJECTION PORTS

Rocket engine with dual contour nozzle

Rocket engine with dual contour nozzle

Rocket propulsion systems and associated methods

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Thrust Augmentation for Liquid Rocket Engines

Rocket propulsion systems and associated methods

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

Rocket engine with integrated oxidizer catalyst in manifold and injector assembly

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Generation of a Pulsed Jet by Jet Vectoring Through a Nozzle with Multiple Outlets

Thrust vector control for hybrid propellants rocket engine with embedded fluid injection ports

Rocket engine's thrust chamber assembly

Electrically operated propellant for solid rocket motor thrust management

Rocket engine bipropellant supply system including an electrolyzer

Method and apparatus for variable exhaust nozzle exit area

Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets

Reactants sprayed into plasma flow for rocket propulsion

Propulsion system with movable thermal choke

Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets

Rocket nozzle and control method for combustion gas flow in rocket engine

Fluidic vectoring for exhaust nozzle

Combustion nozzle fluidic injection assembly

Gas augmented rocket engine

Thrust augmentation in plug nozzles and expansion-deflection nozzles

Deflection system for a gas stream in a nozzle

Fluid vectoring nozzle

Rocket motor nozzle throat area control system and method

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

Asonic aerospike engine

Afterburning turbine exhaust cycle (ABTEC)

Dual mode rocket engine with bipropellant injection in the nozzle

Liquid monopropellant controlled solid rocket motor with aft end injection deflector