STAROVEROV-4 ROCKET ENGINE /VERSIONS/ Russian patent published in 2016 - IPC F02K9/08 F02K9/42 F02K99/00 

FIELD: rocket science.

SUBSTANCE: rocket engine comprises a combustion chamber with a nozzle, into which is forced gaseous or liquid or molten hydride and water or water-based antifreeze, or steam. Molten beryllium hydride 37.93 ± 20 % and water 62.07 ± 20 % are fed into combustion chamber. In compliance with the other version, the rocket engine comprises the body with nozzle. In housing there is hydride or mixture of hydrides and substance or mixture of substances containing water in a bound state. Substances containing water in a bound state used is alum, or silica gel or borax, or magnesium sulphate, or calcium chloride.

EFFECT: higher specific impulse of rocket engine.

5 cl