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Analysis of the project fire re-entry package flow field final technical reportTheoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at hypersonic speeds
Document ID
19650016478
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Byron, S. R.
Foster, R. M.
Hoglund, R. F.
Holt, M.
Kuby, W. C.
Date Acquired
August 2, 2013
Publication Date
October 8, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
U-3020
NASA-CR-63388
Report Number: U-3020
Report Number: NASA-CR-63388
Accession Number
65N26079
Funding Number(s)
CONTRACT_GRANT: NAS1-3419
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GAS FLOW
APOLLO SPACECRAFT
HYPERSONIC SPEED
SPACE VEHICLE
REENTRY

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