FIELD: engines and pumps.
SUBSTANCE: proposed to the surface of the guide means for moving the solid fuel ramjet in the plasma source material from the solid fuel ramjet travel cover glassy film in the form of nanomaterials.
EFFECT: provision of a reliable supply of solid fuel in the plasma source material during continuous operation of the electric rocket engine at low negative temperatures.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ELECTRICAL ROCKET ENGINE | 2013 |
|
RU2551140C2 |
| ARTIFICIAL SATELLITE | 2015 |
|
RU2612312C1 |
| ROCKET ELECTRIC MOTOR | 2002 |
|
RU2225533C2 |
| HYBRID AIR-JET MAGNETOGASDYNAMIC ENGINE | 1998 |
|
RU2138668C1 |
| ENGINE INSTALLATION FOR HYPERSONIC AND AIR SPACE FLYING VEHICLES | 1997 |
|
RU2133863C1 |
| AIRCRAFT POWER UNIT | 2013 |
|
RU2601690C2 |
| COMPOSITE RAMJET ENGINE | 1993 |
|
RU2076829C1 |
| METHOD TO ACCELERATE WORKING MEDIUM FLOW IN ROCKET ENGINE CHANNEL | 1999 |
|
RU2162958C2 |
| HYPERSONIC RAMJET ENGINE | 1996 |
|
RU2116490C1 |
| RAMJET RELATIVISTIC ENGINE | 2020 |
|
RU2776324C1 |
