Comparisons of STS-1 experimental and predicted heating rates
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25582
Reference16 articles.
1. Benchmark aerodynamic heat-transfer data from the first flight of the Space Shuttle Orbiter
2. Approximate heating analysis for the windward-symmetry plane of Shuttle-like bodies at large angle of attack
3. Stagnation and downstream viscous shock-layer solutions with radiation and coupled ablation injection
4. Shuttle /STS-1/ entry trajectory reconstruction
5. Determination of atmospheric properties for STS-1 aerothermodynamic investigations
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