Development of the Mars Science Laboratory Heatshield Thermal Protection System
Author:
Affiliation:
1. NASA Ames Research Center
2. Jet Propulsion Laboratory
3. NASA Langley Research Center
4. Eloret Corporation
5. Lockheed Martin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4229
Reference13 articles.
1. 1Edquist, K.T., Wright, M.J., and Tang, C.Y. "Aerothermodynamic Design Conditions for the Mars Science Laboratory Heatshield,"AIAA-2009-4231,41stAIAAThermophysicsConference,SanAntonio,TX,June22-25,2009.
2. 2Laub, B., Chen, Y. K., Dec, J.A. "Development of a High Fidelity Thermal/Ablation Response Model for SLA-561V," AIAA2009-4231,41stAIAAThermophysicsConference,SanAntonio,TX,June22-25,2009.
3. Post-Flight Analysis of the Stardust Sample Return Capsule Earth Entry
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