| タイトル | NASA Perspective and Modeling of Thermal Runaway Propagation Mitigation in Aerospace Batteries |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150000860 |
| 著者（英） | Shack, P.; Rickman, S.; Button, R.; Iannello, C. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2014-11-19 |
| 言語 | eng |
| 内容記述 | NASA has traditionally sought to reduce the likelihood of a single cell thermal runaway (TR) in their aerospace batteries to an absolute minimum by employing rigorous screening program of the cells. There was generally a belief that TR propagation resulting in catastrophic failure of the battery was a forgone conclusion for densely packed aerospace lithium-ion batteries. As it turns out, this may not be the case. An increasing number of purportedly TR propagation-resistant batteries are appearing among NASA partners in the commercial sector and the Department of Defense. In the recent update of the battery safety standard (JSC 20793) to address this paradigm shift, the NASA community included requirements for assessing TR severity and identifying simple, low-cost severity reduction measures. Unfortunately, there are no best-practice guidelines for this work in the Agency, so the first project team attempting to meet these requirements would have an undue burden placed upon them. A NASA engineering Safety Center (NESC) team set out to perform pathfinding activities for meeting those requirements. This presentation will provide contextual background to this effort, as well as initial results in attempting to model and simulate TR heat transfer and propagation within battery designs. |
| NASA分類 | Fluid Mechanics and Thermodynamics; Electronics and Electrical Engineering |
| レポートNO | GRC-E-DAA-TN19295 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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