Comparison of Orbiter STS-2 development flight instrumentation data with thermal math model predictions
- 7 June 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Space Shuttle Orbiter - Reusable surface insulation flight performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Space Shuttle Orbiter - Reusable surface insulation subsystem thermal performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Use of arc-jet hypersonic blunted wedge flows for evaluating performance of Orbiter TPSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Arc-jet test and analysis of Orbiter TPS inter-tile heating in high pressure gradient flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978