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Charring ablation performance in turbulent flow. Volume 1 - Analytical and experimental studiesSemiempirical correlation techniques for predicting charring ablation performance of Apollo heat shield in turbulent flow
Document ID
19690001488
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Crowder, P. A. (Boeing Co. Seattle, WA, United States)
Del Casal, E. P. (Boeing Co. Seattle, WA, United States)
Gaudette, R. S. (Boeing Co. Seattle, WA, United States)
Date Acquired
August 5, 2013
Publication Date
September 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-65736
D2-114031-1
Report Number: NASA-CR-65736
Report Number: D2-114031-1
Accession Number
69N10819
Funding Number(s)
CONTRACT_GRANT: NAS9-6288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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