Chemical nonequilibrium ablation analysis of MUSES-C super-orbital reentry capsule

Author:

Suzuki Kojiro1,Kubota Hirotoshi1,Fujita Kazuhisa2,Abe Takashi2,Suzuki Kojiro1,Kubota Hirotoshi1,Fujita Kazuhisa2,Abe Takashi2

Affiliation:

1. Tokyo, Univ., Japan

2. Inst. of Space and Astronautical Science, Sagamihara, Japan

Publisher

American Institute of Aeronautics and Astronautics

Cited by 24 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Modeling of Emission Spectra in Nonequilibrium Plasmas for Testing Pyrolyzing Ablators;Journal of Thermophysics and Heat Transfer;2019-10

2. Modeling of Heat Transfer Attenuation by Ablative Gases During the Stardust Reentry;Journal of Thermophysics and Heat Transfer;2015-07

3. Master Equation Analysis of Post Normal Shock Waves of Nitrogen;Journal of Thermophysics and Heat Transfer;2015-04

4. Kinetic Rates for Gas-Phase Chemistry of Phenolic-Based Carbon Ablator in Atmospheric Air;Journal of Thermophysics and Heat Transfer;2015-04

5. Modeling of Strong Nonequilibrium in Nitrogen Shock Waves;44th AIAA Thermophysics Conference;2013-06-22

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