FIELD: engines and pumps, rocket engineering.
SUBSTANCE: rocket engine comprises combustion chamber with nozzle. Liquid metal and water are fed into combustion chamber. Molten beryllium 33.3±20 % and water 66.7±20 % are fed into combustion chamber. According to another version, rocket engine comprises a housing with a nozzle. In housing there is beryllium 20.38 % and crystalline hydrate of magnesium sulphate 79.62 %.
EFFECT: higher specific impulse of rocket engine.
7 cl
| Title | Year | Author | Number |
|---|---|---|---|
| STAROVEROV-4 ROCKET ENGINE /VERSIONS/ | 2012 |
|
RU2586211C2 |
| STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) | 2012 |
|
RU2570913C2 |
| STAROVEROV ROCKET ENGINE (VERSIONS) | 2012 |
|
RU2601820C1 |
| STAROVEROV'S PROPELLANT-6 | 2014 |
|
RU2570010C2 |
| STAROVEROV'S ROCKET ENGINE (VERSIONS) | 2012 |
|
RU2544104C2 |
| STAROVEROV'S-7 ROCKET ENGINE | 2012 |
|
RU2485341C1 |
| STAROVERV'S ROCKET ENGINE-9 (VERSIONS) | 2012 |
|
RU2570910C2 |
| STAROVERV'S ROCKET ENGINE-2 (VERSIONS) | 2012 |
|
RU2570911C2 |
| ROCKET PROPELLANT /VERSIONS/ | 2014 |
|
RU2582712C2 |
| STAROVEROV'S PROPELLANT-20 (VERSIONS) | 2014 |
|
RU2572887C1 |
