| タイトル | Space Station Freedom secondary power wiring requirements |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950009637 |
| 著者（英） | Sawyer, C. R. |
| 著者所属（英） | Boeing Aerospace and Electronics Co. |
| 発行日 | 1994-09-01 |
| 言語 | eng |
| 内容記述 | Secondary power is produced by DDCU's (direct current to direct current converter units) and routed to and through secondary power distribution assemblies (SPDA's) to loads or tertiary distribution assemblies. This presentation outlines requirements of Space Station Freedom (SSF) EEE (electrical, electronic, and electromechanical) parts wire and the approved electrical wire and cable. The SSF PDRD (Program Definition and Requirements Document) language problems and resolution are reviewed. The cable routing to and from the SPDA's is presented as diagrams and the wire recommendations and characteristics are given. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 95N16052 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/109400 |
