FIELD: rocket science.
SUBSTANCE: invention relates to rocket science and concerns a structure of a rocket engine operating on bulk solid fuel. A power mechanism of the rocket engine contains a rotor equipped with a rotation drive, having cells distributed along its periphery, while it contains several rotors distributed along the periphery of a bottom of a working chamber of the rocket engine, while the bottom of the working chamber is equipped with a heat sink made in the form of a heat tube consisting of a vacuumized chamber with liquid and a capillary pump.
EFFECT: invention provides shielding of a bottom of a working chamber from radiation of a combustion area, increase in the quality of combustion processes, as well as reduction in axial dimensions of an engine.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| WORKING CHAMBER OF BULK FUEL ROCKET ENGINE | 2019 |
|
RU2783575C2 |
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RU2752730C1 |
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RU2781321C2 |
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RU2825905C2 |
| FREE-PISTON ENGINE | 2008 |
|
RU2445479C2 |
