FIELD: engines and pumps.
SUBSTANCE: rocket engine combustion chamber operates ad heat exchanger section that preheats fuel flow. Rocket engine incorporates fuel deoxygenating device and combustion chamber fuel-cooled wall communicated with said fuel deoxygenating device. Proposed method consists in fuel desoxygenation, feeding desoxygenated fuel through combustion chamber fuel-cooled wall and, further, from said wall into engine combustion chamber.
EFFECT: increased engine pulse.
10 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET ENGINE | 2003 |
|
RU2266423C2 |
| LIQUID PROPELLANT ROCKET ENGINE ANNULAR CHAMBER | 2008 |
|
RU2403425C2 |
| LIQUID ROCKET ENGINE POWERED BY CRYOGENIC FUEL | 2021 |
|
RU2773694C1 |
| METHOD OF OPERATION OF CLOSED CYCLE LIQUID ROCKET ENGINE WITH AFTERBURNING OF OXIDIZING AND REDUCING GENERATOR GASES WITHOUT COMPLETE GASIFICATION AND LIQUID ROCKET ENGINE | 2022 |
|
RU2801019C1 |
| LIQUID-PROPELLANT ROCKET ENGINE | 2000 |
|
RU2179650C2 |
| ROCKET ENGINE (VERSIONS), ROTOR FOR ROCKET ENGINE (VERSIONS), METHOD OF EXECUTION OF WORKING PROCESSES IN ROCKET ENGINE (VERSIONS) AND METHOD OF COOLING OF ROCKET ENGINE | 2000 |
|
RU2243403C2 |
| LIQUID PROPELLANT ROCKET ENGINE (VERSIONS) | 2006 |
|
RU2301352C1 |
| OPERATION OF OXYGEN-KEROSENE LIQUID ROCKET ENGINE AND ROCKET ENGINE PLANT | 2013 |
|
RU2542623C1 |
| ROCKET NOZZLE AND METHOD TO CONTROL ROCKET ENGINE EXHAUST GAS FLOW | 2008 |
|
RU2383769C1 |
| SYSTEM OF ROCKET ENGINE FOR REALISATION OF HIGH-SPEED RESPONSE | 2010 |
|
RU2531489C2 |
