On Heatshield Shapes for Mars Entry Capsules
Author:
Affiliation:
1. ERC, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-399
Reference26 articles.
1. Mars Exploration Entry, Descent, and Landing Challenges
2. Mars Science Laboratory Entry, Descent, and Landing System
3. Aerothermodynamic Design of the Mars Science Laboratory Heatshield
4. 5Driver, D, Carballo, J, Beck, R, Prabhu, D, Santos, J, Cassell, A, Skokova, K, Tang, C, Hwang, H, Slimko, E, Willcockson, W, Songer, J, "Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System," AIAA-2009-4230.
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