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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