A Collection of Technical Papers: AIAA 11th Thermophysics Conference, San Diego, California, July 14-16, 1976American Institute of Aeronautics and Astronautics, 1976 - Aerothermodynamics |
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ablation absorption AIAA analysis angle applied approximately assumed atmosphere body boundary layer calculated cell coefficient collector conductivity cone configuration considered constant convective cooling coupled determined developed distribution effect energy Engineering entry environment equation evaporation experiment experimental field Figure flight flow fluid flux function given groove heat pipe heat shield heat transfer heating rates included increase indicated initial insulation limit loss mass material measured mechanical method obtained operating optical orbit panel parameters performance phase plate predicted present pressure probe problem properties radiation radiative heating range ratio reference reflectance region relative shape shock shown shows simulation solar solution space spacecraft stabilizer structure surface Table Teflon temperature thermal thickness tion tube values wall wick