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Apollo ablator thermal performance at superorbital entry velocitiesApollo ablator thermal performance at superorbital entry velocities
Document ID
19700029061
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Curry, D. M. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Stephens, E. W. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1970
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-5969
MSC-S-247
Report Number: NASA-TN-D-5969
Report Number: MSC-S-247
Accession Number
70N38377
Funding Number(s)
CONTRACT_GRANT: 914-11-20-11-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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