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Aerodynamic and base heating studies on space shuttle configurationsHeating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamber. Correlation data on windward laminar and turbulent boundary layers and leeside surfaces of the space shuttle orbiter are included.
Document ID
19750012376
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
November 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-120718
AA-2793-Y-2
Accession Number
75N20448
Funding Number(s)
CONTRACT_GRANT: NAS8-24072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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