| タイトル | Electrical Prototype Power Processor for the 30-cm Mercury electric propulsion engine |
| 著者（英） | Biess, J. J.; Frye, R. J. |
| 著者所属（英） | NASA Lewis Research Center|TRW Defense and Space Systems Group |
| 発行日 | 1978-04-01 |
| 言語 | eng |
| 内容記述 | An Electrical Prototpye Power Processor has been designed to the latest electrical and performance requirements for a flight-type 30-cm ion engine and includes all the necessary power, command, telemetry and control interfaces for a typical electric propulsion subsystem. The power processor was configured into seven separate mechanical modules that would allow subassembly fabrication, test and integration into a complete power processor unit assembly. The conceptual mechanical packaging of the electrical prototype power processor unit demonstrated the relative location of power, high voltage and control electronic components to minimize electrical interactions and to provide adequate thermal control in a vacuum environment. Thermal control was accomplished with a heat pipe simulator attached to the base of the modules. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 78A37439
AIAA PAPER 78-684 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/432606 |
