| タイトル | A modular electric power system test bed for small spacecraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950010861 |
| 著者（英） | Button, Robert M.; Baez, Anastacio N. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1994-12-01 |
| 言語 | eng |
| 内容記述 | In the new climate of smaller, faster, and cheaper space science satellites, a new power system topology has been developed at the NASA Lewis Research Center. This new topology is based on a series connected boost converter (SCBC) and can greatly affect the size, weight, fault tolerance, and cost of any small spacecraft using photovoltaic solar arrays. The paper presents electric power system design factors and requirements as background information. The series connected boost converter topology is discussed and several advantages over existing technologies are illustrated. Besides being small, lightweight, and efficient, this topology has the added benefit of inherent fault tolerance. A positive ground power system test bed has been developed for the TROPIX spacecraft program. Performance of the SCBC in the test bed is described in detail. SCBC efficiencies of 95 percent to 98 percent have been measured. Finally, a modular, photovoltaic regulator 'kit' concept is presented. Two SCBC's are used to regulate solar array charging of batteries and to provide 'utilitytype' power to the user loads. The kit's modularity will allow a spacecraft electric power system to be built from off-the-shelf hardware; resulting in smaller, faster, and cheaper spacecraft. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 95N17276
NASA-TM-106812
E-9335
NAS 1.15:106812
AIAA PAPER 95-0030 |
| 権利 | No Copyright |
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