Computational Assessment of Thermal Protection System Damage Experienced During STS-118
Author:
Affiliation:
1. ELORET Corporation, Sunnyvale, California 94086
2. NASA Langley Research Center, Hampton, Virginia 23681
3. NASA Ames Research Center, 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/10.2514/1.40478
Reference12 articles.
1. Columbia Accident Investigation Board Rept., Vol. 1, NASA, Aug. 2003.
2. Orbiter Return to Flight Entry Aeroheating
3. Rapid Aerothermal Simulations of Damage and Repair During a Space Shuttle Mission
4. Computational Aerothermodynamic Assessment of Space Shuttle Orbiter Tile Damage - Open Cavities
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