Analysis of STS-2 experimental heating rates and transition data
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/10.2514/3.25585
Reference22 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. Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination rates
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