Determination of rarefied-flow aerodynamics of the Shuttle orbiter from flight measurements on STS-6 and STS-7
Author:
Affiliation:
1. NASA, Langley Research Center, Space Systems Div., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-347
Reference13 articles.
1. 'Elanchard, R. C. and Rutherford, 3. F. "The Shuttle Orbiter High Resolution Accelerometer Package: Paper 84-0490, January 1984.
2. Direct simulation of transitional flow for hypersonic reentry conditions
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