FIELD: rocket building.
SUBSTANCE: invention refers to rocket propellant for liquid propellant engines. Rocket propellant for liquid propellant engines consists of liquid oxidant, preferably liquid oxygen, and fuel as a solvent of fuel component in the liquid ammonia. According to invention the fuel component is acetylene. At this the concentration of acetylene to liquid ammonia is from 40% to 90% of mass.
EFFECT: invention ensures increase of density impulse of engine thrust by 15-25 kgs-s/kg.
1 dwg, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF INCREASING SPECIFIC IMPULSE OF LIQUID- PROPELLANT ROCKET ENGINE AND ROCKET ENGINE INSTALLATION FOR IMPLEMENTING THIS METHOD | 1998 |
|
RU2146334C1 |
| METHOD TO OPERATE OXYGEN-KEROSINE LIQUID-PROPELLANT ROCKET ENGINES AND FUEL COMPOSITION THEREFOR | 2006 |
|
RU2386845C2 |
| ROCKET PROPELLANT | 2021 |
|
RU2761188C1 |
| METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE AT TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT | 1999 |
|
RU2166661C1 |
| OPERATION OF OXYGEN-KEROSENE LIQUID ROCKET ENGINE AND ROCKET ENGINE PLANT | 2013 |
|
RU2542623C1 |
| LIQUID PROPELLANT ENGINE | 2012 |
|
RU2494274C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2012 |
|
RU2493411C1 |
| METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF OXYGEN OXIDIZER AND HYDROCARBON FUEL AND LIQUID- PROPELLANT ROCKET ENGINE IMPLEMENTING SAID METHOD | 2001 |
|
RU2197628C2 |
| METHOD OF FEEDING THREE-COMPONENT FUEL INTO LIQUID-PROPELLANT ROCKET ENGINE CHAMBER | 2012 |
|
RU2495271C1 |
| METHOD OF FUEL COMPONENTS FEED IN THREE-COMPONENT LIQUID PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER | 2012 |
|
RU2502886C1 |
