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High specific impulse gas-core reactorsCalculated estimates of gas core nuclear rocket engine weights for specific impulses ranging from 3000 to 7000 seconds and for engine thrusts ranging from 4400 to 440,000 newtons
Document ID
19710010425
Document Type
Technical Memorandum (TM)
Authors
Ragsdale, R. G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TM-X-2243
E-6087
Accession Number
71N19900
Funding Number(s)
CONTRACT_GRANT: 122-28
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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