FIELD: space engineering. SUBSTANCE: proposed thermonuclear space engine using for its operation energy of thermonuclear synthesis consists of microthermonuclear reactor with dc electric generator, tank with hydrogen, central and ionic channels enclosed by solenoid coils, ring-shaped cathode and anode of acceleration zone terminating in thrust nozzle. EFFECT: provision of speed in space up to 2•108 m/s.. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BINARY SPACE-VEHICLE ENGINE | 1997 |
|
RU2131998C1 |
| AEROSPACE NUCLEAR ENGINE | 1998 |
|
RU2156378C2 |
| NUCLEAR ROCKET ENGINE | 1995 |
|
RU2113617C1 |
| AVIASPACE ENGINES FOR SPACE AIRCRAFT | 1997 |
|
RU2140014C1 |
| SPACECRAFT ENGINE | 2000 |
|
RU2183764C2 |
| FUSION POWER PLANT | 1998 |
|
RU2156000C2 |
| DEVICE FOR PRODUCTION OF DIAMONDS | 2000 |
|
RU2178435C2 |
| ELECTRIC ROCKET ENGINE | 1996 |
|
RU2121076C1 |
| RAMJET-ELECTRIC ENGINE | 1997 |
|
RU2122651C1 |
| DEVICE FOR PRODUCTION OF DIAMONDS | 2000 |
|
RU2179174C2 |
