Surface Heating Effects of X-33 Vehicle Thermal-Protection-System Panel Bowing
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. Thermosciences Institute, Moffett Field, California 94035
3. BF Goodrich Company, Chula Vista, California 91910
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3522
Reference21 articles.
1. Innovative economic development and technology integration for single stage to orbit (SSTO) concepts
2. X-33 aerothermal environment simulations and aerothermodynamic design
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