FIELD: engines and pumps.
SUBSTANCE: low-thrust rocket engine on hydrogen gas and oxygen comprises a fuel ignition spark plug, a mixing head providing mixing of fuel and internal cooling of the combustion chamber wall, combustion chambers and nozzles, in the air cross-flow of oxygen there are jet nozzles of jet type provided in the mixing head of the engine, the total flow vectors of which are directed in a plane perpendicular to the axis of the engine towards each other.
EFFECT: improved combustion of gaseous hydrogen and oxygen.
4 cl, 1 dwg
