Free-Flight Dynamic Aero Data for a Lifting CEV Capsule-Reference-Cited by-同舟云学术

Free-Flight Dynamic Aero Data for a Lifting CEV Capsule

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Brown Jeffrey¹,Bogdanoff David¹,Yates Leslie²,Chapman Gary¹

Affiliation:

1. ELORET Corporation

2. AerospaceComputing, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1232

Reference31 articles.

1. 2Moseley, William C. Jr., and Martino, Joseph C. "Apollo Wind Tunnel Testing Program - Historical Development of GeneralConfigurations,"NASA TN D-3748,Dec. 1966.

2. 3Malcolm, Gerald N. and Kirk, Donn B. "Comparison of Free-Flight and Conventional Wind-Tunnel Stability Tests for Apollo Command Module and AbortConfigurations," NASA TM X-1137,Sep.1965.

3. 4Moseley, William C. Jr., Moore, Robert H. Jr., and Hughes, Jack E. "Stability Characteristics of the Apollo Command Module,"NASA TN D-3890,Mar.1967.

4. 5CEV Aerosciences Project Aerodynamics Team (Robinson, P., editor), "Orion Aerodynamic Databook, Ver 0.2," NASA ReportNo. JSC-63402,CXP-72167,Jan.2007.

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