Analysis of Afterbody Heating Rates on the Apollo Command Modulels, Part I: AS-202-Reference-Cited by-同舟云学术

Analysis of Afterbody Heating Rates on the Apollo Command Modulels, Part I: AS-202

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:37th AIAA Thermophysics Conference
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Author:

Wright Michael¹,Prabhu Dinesh²,Martinez Edward¹

Affiliation:

1. NASA Ames Research Center

2. Eloret Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2456

Reference42 articles.

1. Jones, R. "Experimental Investigation of the Overall Pressure Distribution, Flow Field, and Afterbody Heat Transfer Distribution ofanApolloReentryConfigurationataMachNumberof8,"NASATMX-813, Jun. 1963.

2. Bertin,J."WindTunnelHeatingRatesfortheApolloSpacecraft,"NASATMX-1033,Jan.1965.

3. Yee, L. "Free-Flight Measurements of Heat Transferred to the Apollo Afterbody with and Without Heat Shield Ablation,"NASATMX-1096,Apr.1965.

4. 3,"NASATND-6792,Apr.1972.

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