Mars Pathfinder Heatshield Design and Flight Experience
Author:
Affiliation:
1. Lockheed Martin Astronautics, Denver, Colorado 80201
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3456
Reference14 articles.
1. Superlight ablative systems for Mars lander thermal protection.
2. Mars Pathfinder six-degree-of-freedom entry analysis
3. Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Database
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