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NUCLEAR ROCKETS FOR TERRESTRIAL AND SPACE MISSIONS

Journal Article · · Planetary Space Sci.
Nuclear rockets are applicable to a wide range of missions from boosting a 100,000 lb payload into space with a single-stage vehicle in the million lb thrust class to a Mars probe or Mars orbiting space vehicle with an initial acceleration of 0.3 g and a thrust of 10,000 lb. A prototype nuclear power plant design is discussed briefly, from which either of the above vehicles may be evolved. The problems involved in launching a nuclear vehicle from the ground and the problems of initiation of flight from a 300 mile Earth orbit are discussed. Some features of terrestrial and space flight peculiar to nuclear propelled vehicles are covered. (auth)
Research Organization:
Thiokol Chemical Corp., Denville, N.J.
NSA Number:
NSA-15-025659
OSTI ID:
4014186
Journal Information:
Planetary Space Sci., Journal Name: Planetary Space Sci. Vol. Vol: 4
Country of Publication:
Country unknown/Code not available
Language:
English