| タイトル | NOAA 26.5 Ah LEO characterization test |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870001660 |
| 著者（英） | Morrow, G. W. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1986-09-01 |
| 言語 | eng |
| 内容記述 | The General Electric (GE) 26.5 Ah NOAA-G flight nickel-cadmium cells were obtained from RCA-Astro Electronics to undergo performance characterization testing at the Goddard Space Flight Center (GSFC). This lot of cells was manufactured with passivated positive plate, to control nickel structure attack duing active material impregnation, and less electrolyte than normal (less than 3cc/Ah). The cells were tested in a parametric low Earth orbit (LEO) cycling regime that was previously used to test and characterize standard 50 Ah cells. Life cycle testing at the Naval Weapons Support Center (NWSC), in Crane, followed. The results of the test showed nominal performance in comparison with previous test data on the standard 50. Life cycle testing in the NOAA orbital regime is continuing at NWSC. |
| NASA分類 | ELECTRONICS AND ELECTRICAL ENGINEERING |
| レポートNO | 87N11093 |
| 権利 | No Copyright |
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