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Analytical study to extend the capabilities of the aerojet-general ablation digital computer program final reportModified computer program mathematical theory and mathematical model description for predicting rocket engine ablative liner thickness, char depth, and temperature distribution
Document ID
19650014067
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carlson, D. K. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 2, 2013
Publication Date
November 1, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-65007
Report Number: NASA-CR-65007
Accession Number
65N23668
Funding Number(s)
CONTRACT_GRANT: NAS9-2832
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MATHEMATICAL MODEL
ABLATING MATERIAL
TEMPERATURE DISTRIBUTION
COMPUTER PROGRAMMING
CHAR

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