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Ablation effects on the Apollo afterbody heat transfer.Apollo afterbody heat transfer, studying ablation effects for various reentry angles of attack
Document ID
19690065691
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lee, G.
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Subject Category
Thermodynamics And Combustion
Accession Number
69A43680
Distribution Limits
Public
Copyright
Other

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