Art
J-GLOBAL ID:202102228119278305   Reference number:21A0057725

Flow Field Analysis around Martian entry capsule by IR emission spectroscopy in expansion tube

膨張波管気流中IR発光分光を用いた火星大気突入機周り流れ場解析
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Material:
Volume: 64th  Page: ROMBUNNO.4F17  Publication year: 2020 
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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Thesaurus term/Semi thesaurus term
Keywords indexed to the article.
All keywords is available on JDreamIII(charged).
On J-GLOBAL, this item will be available after more than half a year after the record posted. In addtion, medical articles require to login to MyJ-GLOBAL.

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Wind tunnel,various testing devices attachment deuices 
Reference (9):
  • Fukuda, Y., Araya, T., Takahashi, Y., Yamada, K., and Koyanagi, J., “Experimental Estimation of Rear-side Heat Flux of Hayabusa Sample Return Capsule,” Aerospace Technology Japan, The Japan Society for Aeronautical and Space Sciences, Vol. 18, pp.127-131, 2019. doi: 10.2322/astj.JSASS-D-18-00024.
  • Fujita, K, Matsuyama, S., Suzuki, T., “Prediction of Forebody and Aftbody Heat Transfer Rate for Mars Aerocapture Demonstrator,” 43rd AIAA Thermophysics Conference, AIAA 2012-3001.
  • Da Silva, M L., Beck, J, “Contribution of CO2 IR Radiation to Martian Entries Radiative Wall Fluxes,” 49th AIAA Aerospace Sciences Meeting, AIAA 2011-135.
  • Cruden, B. A., Brandis, A. M., White, T., R., Mahzari, M., “Radiative Heating for MSL Entry: Verification of Simulations from Ground Test to Flight Data,” 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida, AIAA 2015-1894.
  • Brandis, A. M., Saunders, D. A., Johnston, C., Cruden, B. A., White, T. R., “Radiative Heating on the After-Body of Martian Entry Vehicles,” 45th AIAA Thermophysics Conference, AIAA 2015-3111.
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