Benchmark determination of Shuttle Orbiter entry aerodynamic heat-transfer data
- 1 May 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 20 (3) , 219-224
- https://doi.org/10.2514/3.25583
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Influence of radiant energy exchange on the determination of convective heat transfer rates to Orbiter leeside surfaces during entryPublished 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
- 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
- Flight testing a manned lifting reentry vehicle /Space Shuttle/ for aerothermodynamic performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981