Uncertainty Analysis of Laminar Aeroheating Predictions for Mars Entries
Author:
Affiliation:
1. Eloret Corporation, NASA Ames Research Center, Moffett Field, California 94035
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.20993
Reference24 articles.
1. NASA's In-Space Propulsion Technology Program: Overview and Update
2. Mars Pathfinder trajectory based heating and ablation calculations
3. Wake flow about the Mars Pathfinder entry vehicle
4. Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response
5. Uncertainty and Sensitivity Analysis of Thermochemical Modeling for Titan Atmospheric Entry
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