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Oxidation and sublimation of graphite in simulated re-entry environments.Graphite thermochemical response tested in simulated environment for use as thermal shield for hypersonic reentry vehicles
Document ID
19670041832
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Diaconis, N. S.
Engel, M. J.
Metzger, J. W.
Date Acquired
August 3, 2013
Publication Date
March 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 65-643
Report Number: AIAA PAPER 65-643
Accession Number
67A20561
Funding Number(s)
CONTRACT_GRANT: AF 04/694/-222
CONTRACT_GRANT: SNPC-10
Distribution Limits
Public
Copyright
Other
Keywords
ENVIRONMENT SIMULATION
GRAPHITE
THERMAL PROTECTION
HYPERSONIC REENTRY
REENTRY SHIELD

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