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Thermal protection system performance of the Apollo command module.Thermal protection system for Apollo command module
Document ID
19660048714
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curry, D. M.
Janney, J. M.
Strouhal, G.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Vehicles
Accession Number
66A28004
Distribution Limits
Public
Copyright
Other
Keywords
APOLLO SPACECRAFT
THERMAL PROTECTION
REENTRY EFFECT
SPACECRAFT REENTRY

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