タイトル | The 2kW Mini-BRU Electrical Controls Concept and Transient Performance |
本文(外部サイト) | http://hdl.handle.net/2060/20060008705 |
著者(英) | Birchenough, Arthur G. |
著者所属(英) | NASA Glenn Research Center |
発行日 | 2006-01-01 |
言語 | eng |
内容記述 | The proposed Jupiter Icy Moon Orbiter, JIMO, mission selected a Brayton power conversion system as its electrical power generator. Although the JIMO mission power conversion system was expected to produce in the order of 100 kW, an available 2 kW Brayton system was used to develop control system strategies for the JIMO mission. This report describes the shunt loading voltage/speed regulation control concept developed for the 2 kW system, and the transient performance of controls. The 2 kW alternator is a permanent magnet alternator as proposed for the JIMO mission, and operates at a similar speed and internal impedance, allowing it to be used as an accurate model for performance of the larger system. The JIMO mission was cancelled in September 2005. |
NASA分類 | Electronics and Electrical Engineering |
レポートNO | E-15400 NASA/TM-2006-214043 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/218783 |