LIQUID-PROPELLANT ENGINE AND METHOD OF USE

SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS

Hybrid rocket engine using electric motor-driven oxidizer pump

POWER MODULES FOR HYPERSONIC VEHICLES

SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS

SYSTEM FOR FEEDING LIQUID PROPELLANTS TO COMBUSTION CHAMBER OF AN ENGINE

MICROPUMP-FED AUTOGENOUS PRESSURIZATION SYSTEM

Flow control system for a rocket engine with parallel fuel passage network

Rocket engine bipropellant supply system including an electrolyzer

Method of regulating the pressure within a first rocket engine propellant tank

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

Passive overspeed controlled turbo pump assembly

Engine comprising a rocket combustion chamber and a heat exchanger

Turbopump

Device for powering the pump of a rocket engine using an inertia wheel

Solid propellant gas control system and method

Method and device enabling a rocket engine pump to be driven by an internal combustion engine

Method and a device for calculating a starting or stop sequence for an engine

Device for controlling a regulated system, and an engine including such a device

Rocket engine power cycle

Rocket engine injector

Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems

Propellant volume and mixture ratio control

Thermoelectric rocket propellant tank pressurization system