| タイトル | The Small Explorer power system |
| 著者（英） | Culver, H.; Jagielski, J.; Dakermanji, George; Ahmad, A.; Rodriguez, G. E.; Carlsson, Uno |
| 著者所属（英） | NASA Goddard Space Flight Center|Fairchild Space Co. |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | A direct-energy-transfer (DET) power system design with the battery connected directly to the bus was selected as the generic power system to satisfy the various Small Explorer spacecraft missions. The power system electronics (PSE) are designated to handle power levels up to a 250-W load with minimum changes in the electronics. The command and telemetry interface is through an optical MIL-STD-1773 interface that is contained in the PSE. The system provides high performance, low weight, and low EMI (electromagnetic interference) generation. The design and performance of the power system have been verified through analysis and extensive tests on a breadboard. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 91A37934 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/348167 |
|
