Study on the Electric Propulsion System for Asteroid Detection

Expand
  • Beijing institute of control engineering,Beijing 100190, China

Received date: 07 Jun 2018

Revised date: 12 Jul 2018

Abstract

The electric propulsion has the characteristics of high specific impulse, long service life and highly autonomous cruise, which will significantly reduce the propellant mass and improve the load ratio when it’s used for orbit maneuver operation during the cruise phase of asteroid detection. The electric propulsion system for asteroid detection is investigated. According to the mission requirements of the asteroid detection to the electric propulsion and the technical basis of the existing electric thruster, five kinds of electric propulsion system solutions are proposed and compared, the optimal solution is designed and the key technologies are analyzed.

Cite this article

LI Zongliang, GAO Jun, LIU Guoxi, ZHOU Cheng, TANG Zhangyang, ZOU Daren . Study on the Electric Propulsion System for Asteroid Detection[J]. Journal of Deep Space Exploration, 2018 , 5(4) : 347 -353 . DOI: 10.15982/j.issn.2095-7777.2018.04.004

References

[1] RAWLIN V K,SOVEY J S,HAMLEY J A. An ion propulsion system for NASA’S deep space missions[R]. Albuquerque,New Mexico:AIAA,1999.
[2] THOMAS A B,GERALD B,CARDWELL G I. NSTAR ion engine power processor unit performance:ground test and flight experience[C]//Aerospace Power Systems Conference. USA:[s.n.],1999.
[3] RAYMAN M D. The successful conclusion of the deep space 1 mission:important results without a flashy title[R]. California:Jet Propulsion Laboratory,2003.
[4] KUNINAKA H,SHIMIZU Y,YAMADA T,et al. Flight report during two years on HAYABUSA explorer propelled by microwave discharge ion engines[C]∥The 41th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. [S.l]:AIAA,2005.
[5] NISHIYAMA K,HOSODA S,UENO K,et al. The ion engine system for hayabusa2[C]∥The 32nd International Electric Propulsion Conference. IEPC:[s.n.],2011.
[6] GARNER C E,RAYMAN M D,BROPHY J R. In-flight operation of the dawn ion propulsion system through start of the vesta cruise phase[C]∥The 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. [S.l]:AIAA,2009.
[7] 耿永兵,沈岩,魏延明. 离子推进系统在黎明号探测器上的应用及其思考[J]. 航天器工程,2009,18(5):80-86
GENG Y B, SHEN Y, WEI Y M. Application of ion propulsion system in dawn spacecraft[J]. Spacecraft Enginee-ring,2009,18(5):80-86
Outlines

/