| 摘要 |
A rocket engine comprises an energy converter arranged as steam generator with working chamber, this is connected to source of energy with permanent action, a nozzle connected to sealed balloon, a pump and a pipeline connecting cavity of the balloon to the steam generator. At that additionally it has placed symmetrically pairs of working chambers of steam generator with nozzles and pumps, at that in working chambers of steam generator evaporator is installed, and gates for direction of gas to respective nozzles after which chambers for gas cooling are installed, with cooling ribs on the outer surfaces of those, and the pumps are placed after gas cooling chambers. |
