Technology system of on-orbit strong survivability for GEO satellite bus

被引:0
|
作者
Li W. [1 ]
Kong X. [1 ]
Ma W. [1 ]
Yang L. [1 ]
机构
[1] Shanghai Institute of Satellite Engineering, Shanghai
关键词
Composite warning; Damage effect; Satellite bus; Security protection;
D O I
10.12305/j.issn.1001-506X.2021.03.17
中图分类号
学科分类号
摘要
As high value geostationary earth orbit (GEO) satellites are under a range of threats, it is helpful to improve the survivability of satellite bus by exploring the technology system of on-orbit strong survivability (TSO2S2). Focusing on this, the concept of TSO2S2 is defined systematically. A protection system including warning and safety protection sub-system is built after the main threat sources are figured out. Firstly, 8 threats are divided into active type and passive type. The threat mechanisms are analyzed and the damage effects are evaluated using qualitative and quantitative methods. Secondly, an integrated space and terrestrial warning scheme is proposed and the equipment is designed which enabled 5 types of threats to be alarmed, including space debris, laser, et al. Finally, the protection technology and methods are summarized systematically, which can provide reference for the GEO satellite platform to improve the orbit safety. © 2021, Editorial Office of Systems Engineering and Electronics. All right reserved.
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页码:731 / 739
页数:8
相关论文
共 43 条
  • [1] DOUGLAS V, HARALD W, LOU M., Lockheed Martin's A2100 spacecraft bus modernization, Proc. of the 34th AIAA International Communications Satellite Systems Confe-rence, (2016)
  • [2] MA X B, WEI Q, ZHOU J, Et al., Passive defence system and correlated technology of GEO satellite platform, Aerospace Electronic Warfare, 34, 4, pp. 38-40, (2018)
  • [3] LIU B L, WU M, MA Y W, Et al., Threats to the satellit and its protection, Aerospace Electronic Warfare, 26, 6, pp. 25-27, (2010)
  • [4] LI F Q, CHENG X W, YANG Y, Et al., Technique requirement analysis of satellite borne threat laser detecting warning, Infrared and Laser Engineering, 37, S3, pp. 331-334, (2008)
  • [5] YAN J, ZHENG S G, HAN Z Y, Et al., Space debris protection design and application for Tiangong-1, Scientia Sinica Techologica, 44, 3, pp. 243-250, (2014)
  • [6] DUAN M., Research on damage characteristics of the space debris shield impacted by hypervelocity multiple projectiles, (2018)
  • [7] WU Q, ZHANG Q M, GONG Z Z, Et al., Shielding properties investigation of impact-initiated energetic materials under hypervelocity impact, Proc. of the 7th European Conference on Space Debris, (2017)
  • [8] CHERNIAEV A, TELICHEV I., Sacrificial bumpers with high-impedance ceramic coating for orbital debris shielding: a preliminary experimental and numerical study, International Journal of Impact Engineering, 119, pp. 45-56, (2018)
  • [9] KIM Y H, PARK Y, CHA J H, Et al., Behavior of shear thickening fluid(STF) impregnated fabric composite rear wall under hypervelocity impact, Composite Structures, 204, pp. 52-62, (2018)
  • [10] KIM Y H, CHOI C, KUMAR S, Et al., Behavior of dragon skin flexible metal bumper under hypervelocity impact, International Journal of Impact Engineering, 125, pp. 13-26, (2019)