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Thermochemical ablation.Thermochemical interaction between ablation material and environment during manned reentry, using mainly graphite and composite materials
Document ID
19660030936
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartlett, E. P.
Kendall, R. M.
Rindal, R. A.
Date Acquired
August 3, 2013
Publication Date
September 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 65-642
Report Number: AIAA PAPER 65-642
Accession Number
66A10226
Funding Number(s)
CONTRACT_GRANT: NAS7-218
CONTRACT_GRANT: NAS9-4559
CONTRACT_GRANT: AF 04/611/-9073
Distribution Limits
Public
Copyright
Other
Keywords
REENTRY EFFECT
COMPOSITE MATERIAL
ABLATING MATERIAL
THERMOCHEMISTRY

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