Analysis of Compression Pad Cavities for the Orion Heatshield-Reference-Cited by-同舟云学术

Analysis of Compression Pad Cavities for the Orion Heatshield

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Thompson Richard¹,Lessard Victor²,Jentink Thomas³,Zoby Vincent¹

Affiliation:

1. NASA Langley Research Center

2. Genex Systems

3. ATK Space Division

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1575

Reference10 articles.

1. Liechty, D.S. "Aerothermodynamic Testing ofProtuberancesandPenetrationsonthe NASA Cycle I CrewExploration Vehicle Heat Shieldinthe NASA Langley 20-Inch Mach6 AirTunnel: Test 6918," NASA EG-CAP-06-155

2. Hollis, B.R. "Aerothermodynamic Testing ofRecessed/ Protruding Compression Pads on CEVHeat Shield:LaRC 31-Inch Mach10 Air TunnelTest446," NASA EG-CAP-07-165

3. Hollis, B.R. "Aerothermodynamic Testing ofRecessed/ Protruding Compression Pads on CEVHeat Shield:LaRC 20-Inch Mach6 AirTunnelTest 6946," NASA EG-CAP-07-144

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