ROCKET MOTOR WITH DUAL EMBEDDED BURNABLE CUTTING EXPLOSIVE ENERGETIC MATERIAL

Ballistic Engine

JET ENGINE AND METHOD OF OPERATION

AUXILIARY BOOSTER WITH OPTIMISED ARCHITECTURE

Method of replacing a fan module, engine core module, or fan case module in a gas turbine engine

Satellite with integral thrusters

Generalized jet-effect and enhanced devices

Thruster control device and thruster control method

Variable block shaft for integrated drive generator

Aerospace turbofan engines

Lifting system machine with methods for circulating working fluid

Engine driven by Sc0cycle with independent shafts for combustion cycle elements and propulsion elements

VARIABLE SECTION NOZZLE FOR AIRCRAFT NACELLE AND NACELLE FOR AN AIRCRAFT TURBOJET ENGINE INCLUDING SUCH A NOZZLE

Optical heat exchanger and associated method

Satellite with integral thrusters

Rocket engine bipropellant supply system including an electrolyzer

Vapor jet system enabling jetting for many seconds using multiple kinds of mutually insoluble liquid gases as fuel

Engine driven by SC0cycle with independent shafts for combustion cycle elements and propulsion elements

Electrothermal device for a propulsion system, especially for a turbojet, propulsion system comprising such an electrothermal device, and associated method

Chemical-electromagnetic hybrid propeller with variable specific impulse

Replaceable thrust generating structures attached to an air vehicle

Fuel Cell Powered Jet Engine

Microsatellite comprising a propulsion module and an imaging device

Propulsion device with enclosed plenum

Propulsion device with enclosed plenum

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