Use of arc-jet hypersonic blunted wedge flows for evaluating performance of Orbiter TPS
- 4 June 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Thermal math model analysis of FRSI test article subjected to cold soak and entry environmentsFlexible Reuseable Surface Insulation in Space Shuttle OrbiterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- 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
- Space Shuttle orbiter thermal protection development and verification test programPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Hypersonic viscous interaction on sharp and blunt inclined plates.AIAA Journal, 1969
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961