Ablation Studies for a Super-Orbital Reentry Capsule Using a Three-Temperature Model

Author:

DOIHARA Ryouji,NISHIDA Michio

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference12 articles.

1. VSL Analysis of the Flow Field over a Super Orbital Reentry Capsule.

2. 2) Fujita, K. and Abe, T.: SPRADIAN, Structured Package for Radiation Analysis: Theory and Application, ISAS Report 669, 1997.

3. 3) Inatani, Y. and Ishii, N.: Design Overview of an Asteroid Sample Return Capsule, ISAS Report SP No. 17, 2003, pp. 1–15.

4. Chemical Nonequilibrium Stagnation Ablation Analysis of MUSES-C Superorbital Re-Entry Capsule

5. 5) Blottner, F. G.: Prediction of Electron Density in the Boundary Layer on Entry Vehicles with Ablation, NASA SP-252, 1970, pp. 219–240.

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1. Three-Temperature Thermochemical Nonequilibrium Model with Application to Slender-Body Wakes;Journal of Thermophysics and Heat Transfer;2019-07

2. Simultaneous PIV and PLIF Imaging of Low-Temperature Ablation in a Mach 5 Turbulent Boundary Layer;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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4. Modeling of Stardust Reentry Ablation Flows in the Near-Continuum Flight Regime;AIAA Journal;2008-10

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