FIELD: space engineering. SUBSTANCE: binary space-vehicle engine is just composite compact engine with neutron radiation source in front section which is connected with thermonuclear microreactor changing into central channel. It is coupled with electron rocket engine. Binary space-vehicle engine is provided with liquid hydrogen tank, hydrogen pipe, pump, gas outlet and turbine. Lithium tube with lithium-6 is provided in front section of nuclear engine which is connected with nuclear microreactor through pump and neutron radiation source; nuclear microreactor is connected with central channel terminating in magnetic nozzle forcing-out and accelerating ionized hydrogen. EFFECT: creation of pulse exceeding 3.10 m/s. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
NUCLEAR ROCKET ENGINE | 1995 |
|
RU2113617C1 |
THERMONUCLEAR SPACE ENGINE | 1999 |
|
RU2171914C1 |
AVIASPACE ENGINES FOR SPACE AIRCRAFT | 1997 |
|
RU2140014C1 |
AEROSPACE NUCLEAR ENGINE | 1998 |
|
RU2156378C2 |
FUSION POWER PLANT | 1998 |
|
RU2156000C2 |
ELECTRIC ROCKET ENGINE | 1996 |
|
RU2121076C1 |
SPACECRAFT ENGINE | 2000 |
|
RU2183764C2 |
RAMJET-ELECTRIC ENGINE | 1997 |
|
RU2122651C1 |
METHOD FOR BUILDING UP REACTIVE THRUST OF NUCLEAR ROCKET ENGINE | 1998 |
|
RU2151324C1 |
PLANT FOR PRODUCTION OF HYDROGEN, CARBON BLACK AND DIAMONDS | 1998 |
|
RU2139236C1 |
Authors
Dates
1999-06-20—Published
1997-10-20—Filed