Sensing Aeroheating Flight Experiment - STS-96 flight results
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Computer Sciences Corp., Kennedy Space Center, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-352
Reference11 articles.
1. X-33 hypersonic boundary layer transition
2. Hypersonic boundary layer transition for X-33 Phase II vehicle
3. X-33 experimental aeroheating at Mach 6 using phosphor thermography
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1. High-accuracy infra-red thermography method using reflective marker arrays;Measurement Science and Technology;2017-08-21
2. Coupled CFD/Thermal Response Analysis;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14
3. The crew exploration vehicle (CEV) and the next generation of human spaceflight;Acta Astronautica;2007-06
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