Model for oxygen recombination on silicon-dioxide surfaces. II - Implications toward reentry heating
Author:
Affiliation:
1. Notre Dame, University, IN
2. National Aero-Space Plane Joint Program Office, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-811
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3. Model for oxygen recombination on silicon-dioxide surfaces
4. Rosner, D.E., and Cibrian, R. "Non-Equilibrium Stagnation Region Aerodynamic Heating on Hypersonic Glide Vehicles,"AIAA74-755. 1974.
5. Stewart, D.A., and Rakich, J.V. '"CatalyticSurface Effects Experiment on Space Shuttle,"AIM-81-1143, June 1981.
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