Comparisons of free-flight experimental and predicted heating rates for the Space Shuttle
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Determination of atmospheric properties for STS-1 aerothermodynamic investigationsPublished 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
- Comparison of correlations of Shuttle boundary-layer transition due to distributed roughnessPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Approximate Convective-Heating Equations for Hypersonic FlowsJournal of Spacecraft and Rockets, 1981
- Boundary layer transition flight test observationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Inviscid hypersonic flow past smooth symmetric bodiesAIAA Journal, 1964