Thermophysics of Atmospheric EntryThomas E. Horton |
Contents
Numerical Calculation of Gaseous Transport Properties | 3 |
Transport Properties for a Mixture of the Ablation Products C C₂ | 17 |
Transport Properties Associated with Entry into the Atmosphere | 37 |
Copyright | |
19 other sections not shown
Common terms and phrases
ablation aerobraking aerocapture aerocapture vehicle aerodynamic AIAA AIAA Paper altitude angle of attack approximation atmosphere ballistic coefficient Ballute baseline blunt body boundary boundary-layer bow shock calculated carbon carbon-phenolic catalytic overcoat coefficient collision integrals computed cone configuration convective convective heating core Run correlation density effect enthalpy equations experimental flight flowfield forebody freestream Galileo probe gas mixture heat flux Heat Transfer heat-shield heat-transfer rate heating rates Hypersonic injection interaction inviscid Jovian kg probe km/s laminar Mach number mass driver mass loss material mission N₂ NASA nose radius nosetip obtained Orbiter parameters phenolic potential predicted present pressure radiation radiative heating RASLE re-entry reaction rate constants Reynolds number S/RN shape shock layer shown in Fig simulation solutions species stagnation point surface Table temperature thermal conductivity thermal protection Thermophysics tion trajectory transport properties trip turbulent flow values velocity viscosity windward