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The design of ablative thermal protection systems.Ablative thermal protection system for Apollo command module
Document ID
19650046425
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Erb, R. B.
Kotanchick, J. N.
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Thermodynamics And Combustion
Accession Number
65A29129
Distribution Limits
Public
Copyright
Other
Keywords
THERMAL INSULATION
APOLLO SPACECRAFT
ABLATING MATERIAL
HEAT SHIELD

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