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Hypersonic nonequilibrium flow at re-entry of space vehicles and its thermodynamic relationsHypersonic nonequilibrium flow at reentry of space vehicles and thermodynamic relations
Document ID
19670014951
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hermann, R.
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Space Sciences
Accession Number
67N24280
Funding Number(s)
CONTRACT_GRANT: NSG-381
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMODYNAMIC PROPERTY
HYPERSONIC FLOW
SPACECRAFT REENTRY
NONEQUILIBRIUM FLOW
APOLLO SPACECRAFT
REENTRY EFFECT
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IDRelationTitle19670014939Collected WorksProceedings of the Interdisciplinary Symposium on Apollo Application Programs, 12-13 January 1966N67-24268 12-30Collected Works19670014939Collected WorksProceedings of the Interdisciplinary Symposium on Apollo Application Programs, 12-13 January 1966
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