| タイトル | Use of a New Portable Instrumented Impactor on the NASA Composite Crew Module Damage Tolerance Program |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140016384 |
| 著者（英） | Polis, Daniel L.; Jackson, Wade C. |
| 発行日 | 2014-09-08 |
| 言語 | eng |
| 内容記述 | Damage tolerance performance is critical to composite structures because surface impacts at relatively low energies may result in a significant strength loss. For certification, damage tolerance criteria require aerospace vehicles to meet design loads while containing damage at critical locations. Data from standard small coupon testing are difficult to apply to larger more complex structures. Due to the complexity of predicting both the impact damage and the residual properties, damage tolerance is demonstrated primarily by testing. A portable, spring-propelled, impact device was developed which allows the impact damage response to be investigated on large specimens, full-scale components, or entire vehicles. During impact, both the force history and projectile velocity are captured. The device was successfully used to demonstrate the damage tolerance performance of the NASA Composite Crew Module. The impactor was used to impact 18 different design features at impact energies up to 35 J. Detailed examples of these results are presented, showing impact force histories, damage inspection results, and response to loading. |
| NASA分類 | Composite Materials |
| レポートNO | NF1676L-18063 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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