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Viscous Shock Layer Studies of a Super Orbital Reentry Capsule Using a Multi Vibrational Temperature Model 土井原, 良次 西田, 迪雄 Doihara, Ryouji Nishida, Michio Numerical studies of the shock layer of a super orbital reentry capsule have been conducted by using thermochemical nonequilibrium VSL (Viscous Shock Layer) equations. In the present analysis, vibrational temperature has been treated as individual molecular species vibrational temperature. The analysis has been performed for the MUSES-C reentry conditions, and the temperatures and chemical species mole fractions in the shock layer have been revealed for the typical reentry altitudes of 84 km and 64 km. Radiative heat flux and spectra have been also computed from the results of the VSL analysis to discuss the necessity of the multi vibrational temperature model. Finally, convective heat fluxes for the multi vibrational temperature model and three temperature model are compared. 資料番号: SA0200016000 宇宙科学研究所 Institute of Space and Astronautical Science 2003-03 eng departmental bulletin paper https://jaxa.repo.nii.ac.jp/records/33243 0288-433X AA10455137 The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule 17 83 91 https://jaxa.repo.nii.ac.jp/record/33243/files/SA0200016.pdf application/pdf 2.6 MB 2020-01-24