Mars Pathfinder entry temperature data, aerothermal heating, and heatshield material response
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. Applied Research Associates, Littleton, CO
3. Lockheed Martin Astronautics, Denver, CO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2681
Reference19 articles.
1. Anon. "Aeroshell - 1CD,"JPL Pathfinder design drawing 10158741, Rev.B, July 1995.
2. Mars Pathfinder trajectory based heating and ablation calculations
3. Aerothermal Study of Mars Pathfinder Aeroshell
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