Uncertainty Analysis of Laminar Aeroheating Predictions for Mars Entries
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4682
Reference21 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. Bose, D., Wright, M.J., and Gokcen, T. "Uncertainty and Sensitivity Analysis of Thermochemical ModelingforTitanAtmosphericEntry,"AIAAPaperNo.2004-2455,June2004.
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