Nuclear Thermal Propulsion: Past, Present, and a Look Ahead
NTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission reactor with enriched uranium fuel as thermal power source. Reactor heat is removed using H2 propellant which is then exhausted to produce thrust. Conventional chemical engine LH2 tanks, turbo pumps,...
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| creator | Borowski, Stanley K. |
| description | NTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission reactor with enriched uranium fuel as thermal power source. Reactor heat is removed using H2 propellant which is then exhausted to produce thrust. Conventional chemical engine LH2 tanks, turbo pumps, regenerative nozzles and radiation-cooled shirt extensions used -- NTR is next evolutionary step in high performance liquid rocket engines. |
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| language | eng |
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| source | NASA Technical Reports Server |
| subjects | Spacecraft Propulsion And Power |
| title | Nuclear Thermal Propulsion: Past, Present, and a Look Ahead |
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