Determination of the recombination efficiency of thermal control coatings for hypersonic vehicles
- 1 January 1995
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 32 (1) , 89-96
- https://doi.org/10.2514/3.26579
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Comparison of kinetic models for atom recombination on high-temperature reusable surface insulationJournal of Thermophysics and Heat Transfer, 1993
- Nitrogen recombination on high-temperature reusable surface insulation and the analysis of its effect on surface catalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Vapor-deposited emittance-catalysis coatings for superalloys in heat-shield applicationsJournal of Thermophysics and Heat Transfer, 1987
- Catalytic recombination of nitrogen and oxygen on high-temperature reusable surface insulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Stagnation-point convective heat transfer in frozen boundary layers.AIAA Journal, 1968
- On Catalytic Recombination Rates in Hypersonic Stagnation Heat TransferJournal of Jet Propulsion, 1958
- The kinetics of the recombination of oxygen atoms at a glass surfaceProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1956
- Heat TransferIndustrial & Engineering Chemistry, 1949