STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) Russian patent published in 2015 - IPC F02K9/08 F02K9/42 F02K99/00 

FIELD: engines and pumps.

SUBSTANCE: claimed engine comprises the combustion chamber with nozzle. Molten beryllium hydride in amount of 40.81±20 wt % and oxygen in amount of 59.19±20 wt % the components are added at the following ratio: diborane - 10.10 wt %, beryllium hydride - 24.16 wt %, nitric acid - 23.0 wt % and methane - 42.74 wt %. In compliance with the other version, the rocket engine comprises the body with nozzle. Said body houses the hydride or the mix of hydrides and the substance or the mix of substances containing the bound oxygen in the amount that makes the hydrogen release in the reaction. Note here that said rocket engine is exploited as the hydrogen-releasing grain for liquid- or solid-propellant engine.

EFFECT: higher specific thrust pulse.

11 cl