FIELD: engines and pumps.
SUBSTANCE: proposed method proceeds from gasification of rocket propellant components (RPC) to be fed into combustion chamber. Note here that after outage of liquid-propellant mid-flight engine RPC gasification system is actuated. Supercharge gas is fed into balloons with extra RPC. Redox gas generators are used to feed heat carriers into tanks with RPC residues depending upon specific fuel kept in tanks.
EFFECT: higher power efficiency and environmental safety, better operating performances.
1 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| REALIZATION METHOD OF ROCKET POWER AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2614271C2 |
| INCREASING EFFICIENCY OF SPACE ROCKET WITH MID-FLIGHT LIQUID-PROPELLANT ENGINE | 2014 |
|
RU2562826C1 |
| WITHDRAWAL OF CARRIER ROCKET STAGE SEPARATED PART FROM PAYLOAD ORBIT AND DEVICE TO THIS END | 2012 |
|
RU2518918C2 |
| METHOD OF ROCKET IN-TANK LIQUID-PROPELLANT GASIFICATION AND DEVICE TO THIS END | 2012 |
|
RU2522536C1 |
| METHOD OF DRIVING CARRIER ROCKET SEPARABLE UNIT FROM PAYLOAD ORBIT AND DEVICE TO THIS END | 2011 |
|
RU2482034C1 |
| METHOD FOR SIMULATING PROCESS OF COMBUSTION OF PRODUCTS OF GASIFICATION OF LIQUID ROCKET FUEL COMPONENT RESIDUES AND DEVICE THEREFOR | 2015 |
|
RU2588343C1 |
| METHOD OF THE LIQUID OXYGEN AND KEROSENE UNPROCESSED RESIDUES GASIFICATION IN THE BOOSTER ROCKET TANKS AND THE DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2654235C1 |
| METHOD OF LOWERING THE SPENT PART OF SPACE-MISSION VEHICLE SUBMISSILE AND THE DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2621771C2 |
| METHOD OF WITHDRAWING ROCKET CARRIER SEPARATED SECTION (RCSS) FROM PAY LOAD ORBIT AND POWER PLANT TO THIS END | 2008 |
|
RU2406856C2 |
| METHOD OF DESCENDING SEPARATED SPACE ROCKET STAGE AND DEVICE THEREFOR | 2015 |
|
RU2581894C1 |
