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J-GLOBAL ID:201802212696760616   Reference number:18A2092117

Safety evaluation and injury mechanism identification in launch abort system using finite element method

有限要素法を用いた有人ロケット緊急離脱時における人体傷害評価及び脳傷害メカニズム解明
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Material:
Volume: 84  Issue: 866  Page: ROMBUNNO.18-00126(J-STAGE)  Publication year: 2018 
JST Material Number: U0182B  ISSN: 2187-9761  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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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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Category name(code) classified by JST.
Biometry  ,  Operating technology 
Reference (24):
  • AAAM, Abbreviated injury scale 2005 update 2008, Barrington Illinois, Association for the Advancement of Automotive Medicine (2008).
  • Adams, J. H., Graham, D. I., Gennarelli, T. A. and Maxwell, W. L., Diffuse axonal injury in non-missile head injury, Journal of neurology, neurosurgery, and psychiatry, Vol. 54 (1991), pp. 481-483.
  • Antona-Makoshi, J., Davidsson, J., Ejima, S., Ono, K., Brolin, K. and Anata, K., Correlation of global head and brain tissue injury criteria to experimental concussion derived from monkey head trauma experiments, IRCOBI Conference 2013, IRC-13-55 (2013), pp. 509-522.
  • Eppinger, R., Sun, E., Bandak, F., Faffner, M., Khaewpong, N., Maltese, M., Kuppa, S., Nguyen, T., Takhounts, T., Tannous, R., Zhang, A. and Saul, R., Development of improved injury criteria for the assessment of advanced automotive restraint systems-II, National Highway Traffic Safety Administration (1999).
  • Fujimoto, K., Wada, E. and Tani, N., Quantitative crew safety analysis for launch abort system, in 1st International Conference on Computational Engineering and Science for Safety and Environmental Problems (2014), pp. 416-419.
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