The three-component liquid rocket launcher cryogenic environmentally friendly components

摘要

The invention relates to the field of rocket technology, in particular to the design of rocket motors to cryogenic fuels. Rocket propulsion unit comprising a liquid-propellant rocket engine, the oxidizer tank and a fuel tank, the ball-cylinder of compressed gas and pipes with shut-off and control valves, characterized in that the oxidizer tank filled with hydrogen peroxide, the fuel tank is filled with a mixture of ammonia and acetylene, with this fuel tank and the oxidizer tank made of composite material, and the oxidant tank further comprises a thin-walled aluminum liner, Installation, characterized in that the ball-balloon filled with helium. Using the utility model can increase specific impulse propulsion system. 2 h. n. f ly-1-yl.