Mars Science Laboratory Heatshield Development, Implementation, and Lessons Learned
Author:
Affiliation:
1. Entry, Descent, and Landing Systems & Advanced Technologies Group, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
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.A32673
Reference7 articles.
1. MSL heatshield development: From failure to success
2. Aerothermodynamic Design of the Mars Science Laboratory Heatshield
3. Development of the Mars Science Laboratory Heatshield Thermal Protection System
4. Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System
5. Development of a High-Fidelity Thermal/Ablation Response Model for SLA-561V
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