Analysis of STS-2 experimental heating rates and transition data
- 1 May 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 20 (3) , 232-237
- https://doi.org/10.2514/3.25585
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Comparisons of free-flight experimental and predicted heating rates for the Space ShuttlePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Benchmark aerodynamic heat-transfer data from the first flight of the Space Shuttle OrbiterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Determination of atmospheric properties for STS-1 aerothermodynamic investigationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Shuttle /STS-1/ entry trajectory reconstructionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Space Shuttle laminar heating with finite-rate catalytic recombinationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Approximate heating analysis for the windward-symmetry plane of Shuttle-like bodies at large angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Approximate Convective-Heating Equations for Hypersonic FlowsJournal of Spacecraft and Rockets, 1981
- Stagnation and downstream viscous shock-layer solutions with radiation and coupled ablation injectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Inviscid hypersonic flow past smooth symmetric bodiesAIAA Journal, 1964