Temperature-dependent reaction-rate expression for oxygen recombination at Shuttle entry conditions
Author:
Affiliation:
1. NASA, Langley Research Center, Space Systems Div., Hampton, VA
2. NASA, Langley Research Center,Hampton; Old Dominion University, Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-224
Reference20 articles.
1. Catalytic recombination and Space Shuttle heating
2. Results of a flight experiment on the catalytic efficiency of the Space Shuttle heat shield
3. and Catalysis on Shuttle Heat Transfer,'' AIM -i Paper 83-1485, June 1983.
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