| タイトル | The Use of a Vehicle Acceleration Exposure Limit Model and a Finite Element Crash Test Dummy Model to Evaluate the Risk of Injuries During Orion Crew Module Landings |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080018587 |
| 著者（英） | Brinkley, James W.; Shemwell, David M.; Tabiei, Ala; Lawrence, Charles; Fasanella, Edwin L. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2008-04-01 |
| 言語 | eng |
| 内容記述 | A review of astronaut whole body impact tolerance is discussed for land or water landings of the next generation manned space capsule named Orion. LS-DYNA simulations of Orion capsule landings are performed to produce a low, moderate, and high probability of injury. The paper evaluates finite element (FE) seat and occupant simulations for assessing injury risk for the Orion crew and compares these simulations to whole body injury models commonly referred to as the Brinkley criteria. The FE seat and crash dummy models allow for varying the occupant restraint systems, cushion materials, side constraints, flailing of limbs, and detailed seat/occupant interactions to minimize landing injuries to the crew. The FE crash test dummies used in conjunction with the Brinkley criteria provides a useful set of tools for predicting potential crew injuries during vehicle landings. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | E-16469
NASA/TM--2008-215198 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/256064 |
