STAROVEROV - 5 ROCKET ENGINE /VERSIONS/

摘要

FIELD: engines and pumps, rocket engineering.SUBSTANCE: rocket engine comprises combustion chamber with nozzle. Liquid metal and water are fed into combustion chamber. Molten beryllium 33.3±20 % and water 66.7±20 % are fed into combustion chamber. According to another version, rocket engine comprises a housing with a nozzle. In housing there is beryllium 20.38 % and crystalline hydrate of magnesium sulphate 79.62 %.EFFECT: higher specific impulse of rocket engine.7 cl