期刊文献+

适用于30cm离子推力器的5kW电源处理单元设计 被引量:11

Design of a 5kW Modular Power Processing Unit for 30cm Ion Thruster
下载PDF
导出
摘要 为了满足更大范围的卫星应用需求,我国正在研制30cm离子推力器。30cm离子推力器瞄准全电推进卫星平台、近深空探测器对推进任务的需求,对提高卫星平台先进性和提升国际竞争力具有重要的意义。为了配合30cm离子推力器的研制,同时设计了输出功率达到5kW的电源处理单元。该设计实现了一种输出功率为1kW的模块,通过串联组合可以达到输出5kW功率要求,提出了一种"最佳"的平顶变换及软开关的全桥电路拓扑,达到了95%的转换效率,同时还能容易实现屏栅电源的N+1冗余设计。并且通过高压组件的完全灌封,有效提高产品的可靠性。 To broaden mission applications, a 30cm Ion Thruster has been developed. The 30cm Ion Thruster, which is to be applicable to full electric propulsion satellite platform and near deep- space missions, have importance in raising satellite platform technique and promoting international competitiveness. For development of the 30cm Ion Thruster, a 5kW power processing unit is designed. The design includes several lkW power modules which are connected in series to achieve 5kW output power, puts forward a kind of "Optimum" Flattop conversion and full bridge soft-switching topology, realizes 95 percent conversion efficiency, as well as implements N+I redundant beam supply. Also the high voltage components are completely potted to improve product reliability effectively.
出处 《航天器工程》 2013年第5期74-79,共6页 Spacecraft Engineering
关键词 电推进 30 cm离子推力器 5 kW电源处理单元 高效率 electric propulsion 30cm ion thruster 5kW power processing unit~ high-efficiency
  • 相关文献

参考文献7

  • 1Gollor M,Boss M. Electric propulsion electronics activities in Astrium Germany,IEPC-2007-20[A].Washington D.C.:AIAA,2007.
  • 2Meusemann H,Winter M. Electric propulsion in Germany:current program and prospective,IEPC-2005-130[A].Washington D.C.:AIAA,2005.
  • 3Pi(n)ero L R,Bond T,Okada D. Design of a modular 5kW power processing unit for the next-generation 40cm Ion engine,NASA/TM-2002-211359[R].{H}Washington,DC:NASA,2002.
  • 4Gollor M,Boss M,Herty F. Generic high voltage power supplies (HVPS) with optimum efficiency and multi-range[A].Washington D.C.:AIAA,2007.
  • 5Gollor M,Boss M. Generic high voltage power supplynext generation[A].Washington D.C.:AIAA,2006.
  • 6Boss M,Herty F,Rogalla K. Generic high voltage power module for electrical propulsion,IEPC-2005-278[A].Washington D.C.:AIAA,2005.
  • 7Pi(n)ero L R,Hopson Mark,Todd P C. Performance of the NEXT engineering model power processing unit,AIAA 2007-5214[A].Washington D.C.:AIAA,2007.

同被引文献53

引证文献11

二级引证文献20

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部