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Preliminary Mach 6 aim test results. Hypersonic research engine project-phase 2
Document ID
19800073781
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 10, 2013
Publication Date
January 30, 1974
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-163016
Report Number: NASA-CR-163016
Accession Number
80N73872
Funding Number(s)
CONTRACT_GRANT: NAS1-6666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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