FIELD: engines and pumps.
SUBSTANCE: invention relates to rocket engine production. The proposed rocket liquid propellant engine comprises a combustion chamber with a cooling circuit and jet head, gas generator, fuel pump, oxidiser pump and the turbine with its intake communicating the gas generator and its outlet communicating with the jet head. Note here that it comprises additional turbine with its intake communicating with the cooling circuit outlet and its outlet communicating with the jet head.
EFFECT: higher reliability and longer life.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LIQUID PROPELLANT ROCKET ENGINE | 2014 |
|
RU2545613C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2011 |
|
RU2476709C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2013 |
|
RU2514582C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2011 |
|
RU2476706C1 |
| LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2466292C1 |
| LIQUID FUEL ROCKET MOTOR | 2013 |
|
RU2531831C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2011 |
|
RU2476708C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2012 |
|
RU2495273C1 |
| THREE-COMPONENT LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2484287C1 |
| LIQUID-PROPELLANT ROCKET ENGINE FUEL FEED PLANT | 2014 |
|
RU2574192C1 |
