Transition Due to Heat-Shield Cavities on a Mars Entry Vehicle
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.19669
Reference26 articles.
1. Entry Configurations and Performance Comparisons for the Mars Smart Lander
2. Mars Science Laboratory Experimental Aerothermodynamics with Effects of Cavities and Control Surfaces
3. Aeroheating Environments for a Mars Smart Lander
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