Preliminary Analysis of the Mars Science Laboratory's Entry Aerothermodynamic Environment and Thermal Protection System Performance
Author:
Affiliation:
1. Georgia Institute of Technology
2. ERC, Inc.
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-185
Reference33 articles.
1. A Review of Aerothermal Modeling for Mars Entry Missions
2. Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design
3. Viking Afterbody Heating Computations and Comparisons to Flight Data
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