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A design and performance study of the nuclear direct-air-cycle supersonic airplane, including the effects of operating temperatures and fuel plate material and thickness
Author:
Manson, S. V.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53C18
Link:
https://digital.library.unt.edu/ark:/67531/metadc59760/
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