期刊文献+

登陆火星飞船“推进系统”的遴选及其物理学性能

THE COMPREHENSIVE OPTION OF THE SPACECRAFT PROPULSION SYSTEMS USING FOR LANDING ON MARS AND ITS PHYSICAL PERFORMANCE
下载PDF
导出
摘要 以美国为首的火星登陆计划正受到越来越多的关注."火星之旅"中关键环节是顺利将人类送抵火星.对于火星探测载人飞船,整个飞行过程中需要突破的关键性技术之一是飞船推进系统.文章介绍几种目前在此项目中被广泛接受的飞船推进系统,从物理学原理角度分析飞船推进过程中轨道选择等问题,对几种飞船推进系统及其物理学参数进行了全面的比较和分析,以及飞船推进系统的最佳选择等,以飨读者. The Mars landing project led by the United States has drawn more and more atten- tion recently. The key point in the trip to Mars is to send humans to Mars successfully. For the manned spacecraft to Mars, one of the key technology breakthroughs is the propulsion systems of spacecraft. In this paper, several propulsion systems of spacecraft widely accepted in this project are introduced. Based on the physical principles, the track selection problem during the process of spacecraft propulsion are discussed. Besides, several kinds of spacecraft propulsion systems and their physics parameters are comprehensively compared and analyzed. The best choice of spacecraft propulsion system is also suggested, as a reference for the read- ers.
出处 《物理与工程》 2016年第1期58-63,共6页 Physics and Engineering
基金 中国农业大学教育教学改革项目 多层次的"大学物理"国际化教育教学模式与学生科研能力的培养(201416) 2014年中国农业大学本科生科研训练计划项目:以大学物理双语教学为载体对学生科研能力的培养
关键词 火星登陆 推进器 可变比冲磁等离子体火箭(VASIMR) 核动力 无工质微波推力器 Mars landing propeller variable specific impulse magnetoplasma rocket (VA- SIMR) nuclear power propellantless microwave thrusters
  • 相关文献

参考文献12

二级参考文献58

  • 1吴汉基,安世明.俄罗斯等离子体发动机的研究和应用[J].中国航天,1993(9):40-43. 被引量:5
  • 2邱孝明,唐德礼,孙爱萍,刘万东,曾学军.Role of on-board discharge in shock wave drag reduction and plasma cloaking[J].Chinese Physics B,2007,16(1):186-192. 被引量:6
  • 3吴汉基.脉冲等离子体电火箭在卫星控制方面的应用[J].电工电能新技术,1986,(3):27-33.
  • 4[1]Chang Díaz F R.The VASIMR Engine[J].Scientific American,2000,283:72-79.
  • 5[2]Chang Díaz F R.An overview of the VASIMR engine:High power space propulsion with RF plasma generation and heating[C].Proceedings of Radio Frequency Power in Plasmas:14th Topical Conference,2001:3-15.
  • 6[3]Squire J P,Chang Díaz F R,Jacobson V T,et al.Helicon plasma injector and ion cyclotron acceleration development in the VASIMR experiment[R].AIAA 2000-3752.
  • 7[4]Rey C M,Hoffman W C,Chang Díaz F R,et al.Design and fabrication of an HTS magnet for the VASIMR experiment[J].IEEE Transactions on Applied Superconductivity,2002,12:993-996.
  • 8[5]Glover T W,Chang Díaz,F R,Squire J P,et al.Principal VASIMR results and present objectives[R].Space Technology and Applications International Forum,2005.
  • 9[6]Bering E A Ⅲ,Squire J P.Progress toward the development of a 50 kW VASIMR engine[R].AIAA 2005-0369.
  • 10[7]Ilin A V,Chang Díaz F R,Squire J P,et al.Plasma heating simulation in the VASIMR system[R].AIAA 2005-0949.

共引文献128

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