| タイトル | Electrical Auxiliary Power Unit (EAPU) Corona Design Guideline |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040139579 |
| 著者（英） | Hillard, Barry; Kirkici, Hulya; Dunbar, William; Hall, David K.; Schweickart, Dan L. |
| 著者所属（英） | Air Force Research Lab.; NASA Marshall Space Flight Center; NASA Johnson Space Center; NASA Glenn Research Center |
| 発行日 | 2000-06-29 |
| 言語 | eng |
| 内容記述 | This document is the result of a collaborative effort between NASA's Johnson Space Center, Marshall Space Flight Center, Glenn Research Center, and the United States Air Force Research Laboratory at Wright Patterson AFB in support of the Space Shuttle Orbiter Upgrades Program, specifically the Electric Auxiliary Power Unit Program. This document is intended as a guideline for design applications for corona and partial discharge avoidance and is not a requirements specification instrument. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | JSC-29129-Rev |
| 権利 | No Copyright |
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