Reconstruction of Mars Pathfinder Aeroheating and Heat Shield Response Using Inverse Methods
Author:
Affiliation:
1. Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
2. Aerothermodynamics Branch, ERC, Inc., Moffett Field, California 94035
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.A32462
Reference27 articles.
1. A Review of Aerothermal Modeling for Mars Entry Missions
2. Overview of the MEDLI Project
3. Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response
4. Data-Parallel Line Relaxation Method for the Navier-Stokes Equations
5. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
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