Turbulent Aeroheating Testing of Mars Science Laboratory Entry Vehicle in Perfect-Gas Nitrogen
Author:
Affiliation:
1. NASA Langley Research Center
2. Arnold Engineering Development Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1208
Reference19 articles.
1. Introduction: Mars Science Laboratory: The Next Generation of Mars Landers
2. Entry Configurations and Performance Comparisons for the Mars Smart Lander
3. 3Edquist, K. T. "Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule," AIAA Paper 2007-1206,45thAIAAAerospaceSciencesMeeting andExhibit,Reno,NV,Jan.8-11,2007.
4. Transition Due to Heat-Shield Cavities on a Mars Entry Vehicle
5. Mars Science Laboratory Experimental Aerothermodynamics with Effects of Cavities and Control Surfaces
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