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Apollo experience report: Aerothermodynamics evaluationThe Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superorbital velocities on full-scale spacecraft. Four unmanned flight tests were conducted to qualify the Apollo command module heat shield. Aerothermodynamic measurements were made, and data are presented to illustrate the comparison of the flight data with the ground-test results and theoretical predictions.
Document ID
19720018273
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lee, D. B.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
MSC-S-287
NASA-TN-D-6843
Accession Number
72N25923
Funding Number(s)
PROJECT: RTOP 914-11-20-10-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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