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J-GLOBAL ID:201702230112691849   Reference number:17A1613537

Prediction of the measured radiative intensities around Martian entry model in the hyper velocity expansion tube

膨張波管試験における火星大気突入機周り輻射場の数値解析による再現
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Volume: 61st  Page: ROMBUNNO.2J07  Publication year: 2017 
JST Material Number: S0277B  ISSN: 1884-1945  Document type: Proceedings
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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Aerodunamics of space crafts 
Reference (8):
  • Satoh, T., Kubota, T., Okada, T., Matsuoka, A., Imamura, T., Ogawa, N., Miyamoto, H., Terada, N., Seki, K. and Fujita, K., “Japan’s Mars Exploration with an Lander and Orbiters (MELOS): An Over-view,” Proceedings of 27th International Symposium on Space Technology and Science, ISTS Paper 2009-k-22, Tsukuba, Japan, 2009.
  • Takayanagi, H., Nomura, S., and Fujita, K., “Emission intensity measurement around Mars entry capsule with a free piston driven expansion tube,” AIAA paper 2014-0516, 2014.
  • Takayanagi, H., Nomura, S., Lemal, A., and Fujita, K., “Measurements of nonequilibrium carbon dioxide infrared radiation in an expansion tube,” AIAA paper 2017-1369, 2017.
  • 藤田和央, 鈴木俊之, 松山新吾, “ JAXA汎用高エンタルピー非平衡流れ解析コードの開発,”日本流体力学会年会, 2009.
  • Yamada, T., Lemal, A., Matsuyama, S., Nomura, S., Takayanagi, H., Fujita, K., and Matsui, M., ”Numerical simulation of flow conditions generated by hyper velocity expansion tube,” Proceedings of the 30th International Symposium on Space Technology and Science, Matsuyama city, Japan, July 3rd -9th 2017
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