| タイトル | Hypervelocity Impact Testing of Nickel Hydrogen Battery Cells |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970001594 |
| 著者（英） | Nahra, Henry K.; Frate, David T. |
| 著者所属（英） | NASA |
| 発行日 | 1996-09-01 |
| 言語 | eng |
| 内容記述 | Nickel-Hydrogen (Ni/H2) battery cells have been used on several satellites and are planned for use on the International Space Station. In January 1992, the NASA Lewis Research Center (LeRC) conducted hypervelocity impact testing on Ni/H2 cells to characterize their failure modes. The cell's outer construction was a 24 mil-thick Inconel 718 pressure vessel. A sheet of 1.27 cm thick honeycomb was placed in front of the battery cells during testing to simulate the on-orbit box enclosure. Testing was conducted at the NASA White Sands Test Facility (WSTF). The hypervelocity gun used was a 7.6 mm (0.30 caliber) two-stage light gas gun. Test were performed at speeds of 3, 6, and 7 km/sec using aluminum 2017 spherical particles of either 4.8 or 6.4 mm diameter as the projectile. The battery cells were electrically charged to about 75 percent of capacity, then back-filled with hydrogen gas to 900 psi simulating the full charge condition. High speed film at 10,000 frames/sec was taken of the impacts. Impacts in the dome area (top) and the electrode area (middle) of the battery cells were investigated. Five tests on battery cells were performed. The results revealed that in all of the test conditions investigated, the battery cells simply vented their hydrogen gas and some electrolyte, but did not burst or generate any large debris fragments. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | 97N11388
NASA-TM-107325
NAS 1.15:107325
AIAA Paper 96-4292
E-10431 |
| 権利 | No Copyright |
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