期刊文献+

离子束推移清除空间碎片技术浅析

An Analysis of Space Debris Removal with Ion Beam Deorit Technology
下载PDF
导出
摘要 离子束推移离轨技术是一种新型的非接触式空间碎片清除方式,适合于远距离操作,不需要交会过程和复杂的控制系统,适合于不同尺寸大小的空间碎片。目前,欧空局、日本、俄罗斯都提出了类似的概念。本论文从技术可行性、关键技术、优缺点等方面对离子束推移离轨技术开展了分析。 Ion beam deorbit technology is a new non-contact method of space debris removal.It is suitable for long-distance operation, no need to rendezvous and complicated control system.It is fit for different sizes of space debris.Nowadays, ESA, Japan,Russia all put forward the similar conceptions.This thesis shows an analysis of ion beam technology from several aspects, such as technical feasibility, key technologies, advantages and disadvantages.
作者 陈蓉 申麟 唐庆博 肖肖 童科伟 CHEN Rong;SHEN Lin;TANG Qingbo;XIAO Xiao;TONG Kewei(R&D Center of China Academy of Launch Vehicle Technology,Beijing 100076,China)
出处 《空间碎片研究》 2018年第1期48-52,共5页 Space Debris Research
关键词 离子束推移 空间碎片 清除 非接触 ion beam push to deorbit space debris non-contact
  • 相关文献

参考文献1

二级参考文献37

  • 1KESSI,ER D J,COUR-PALAIS B G. Collision frequency of artificial satellites :The creation of a debris beh[ J ]. Journal of Geophysical Research: Space Physics, 1978,83 ( A6 ) : 2637 -2646.
  • 2VENIAMINOV S S,CHERVONOV A M. Kosmicheskii mu- sor-ugroza cheloveehestvu [ J ]. Space Debris : Threat to Hu- manity ), Moscow : Institute of Space Research of Russian A- cademy of Sciences,2012 : 192.
  • 3BONNAI, C, RUAULT J M, DESJEAN M C. Active debris removal: Recent progress and current trends [ J ]. Acta As- tronautica,2013,85:51-60.
  • 4WIEDEMANN C, FLEGEL M, MOCKEL M. Active space debris removal, in : Deutscher Luft- und Raumf'ahrtKon,n'ess [ Z]. Berlin, Germany,2012.
  • 5PERGOI,A P, RUGGIERO A,ANDRENUCCI M,et al. Ex- panding foam application for active space debris removal systems [ C ]//Proceedings,62nd International Astronautical Congress IAC11, IAC-I 1 A. 2011,6.
  • 6PERGOLA P, RUGGIERO A, ANDRENUCCI M, et al. low- thrust Missions for Expanding Foam Space Debris Removal [ C ]//International Electric Propulsion Conference. 2011.
  • 7NOCK K T,GATES K L,AARON K M,et al. Gossamer Or- bit Lowering Device (GOLD) for safe and efficient de-orbit [ C ]//A1AA Astrndynamics Specialists Conference. 2010.
  • 8ROBINSON E Y. Spacecrt for removal of space orbital debris[ P]. U. S. Patent :6,655,637,2003-12-2.
  • 9WRIGHT R J. Orbital debris mitigation system and method [ P]. U. S. Patent: US8567725,2013435-13.
  • 10WILLIAMS P. Optimal Orbit Transfer with ElectrodynamicTether[ J ]. Journal of Guidance Control & Dynamics,2005, 28(2) :369-371.

共引文献8

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