Safety evaluation and injury mechanism identification in launch abort system using finite element method-Reference-Cited by-同舟云学术

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

Published:2018 Issue:866 Volume:84 Page:18-00126-18-00126
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

UEDA Akihiro¹,IMAIZUMI Shunsuke¹,NAKAGAWA Kodai¹,FUJIMOTO Keiichiro²,HATANO Asuka¹,IZUMI Satoshi¹,SAKAI Shinsuke¹

Affiliation:

1. Department of Mechanical Engineering, The University of Tokyo

2. Japan Aerospace Exploration Agency, Research and Development Directorate, Research Unit III

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/84/866/84_18-00126/_pdf

Reference24 articles.

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3. 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.

4. 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).

5. 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.