Article

Application Scheme of Ion Electric Propulsion System for Main-Belt Asteroid Sample and Return Mission

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  • 1. Lanzhou Institute of Physics, Lanzhou 730000, China
    2. Shanghai Institute of Satellite Engineering, Shanghai 210000, China

Received date: 16 Jan 2015

Revised date: 23 Jun 2015

Published date: 20 May 2022

Abstract

Due to the ion electric propulsion high specific impulse feature, the launch weight of the spacecraft will be greatly reduced under the same payload to implement the orbit maneuver of an asteroid exploration. The application of ion electric propulsion in deep space exploration is investigated in this paper. On the basis of the successful experience of foreign countries and the analysis of the requirements of the task, the scheme and application strategy of the ion electric propulsion system are designed, and its thrust,specific impulse, propellant weight and power are calculated for the main-belt asteroid exploring spacecraft to meet the present life level of ion thruster. The research results show that the developing ion thruster can meet the requirements of the main-belt asteroid exploration mission and have reference value for the design of the spacecraft.

Cite this article

YANG Fuquan, ZHAO Yide, LI Juan, GENG Hai, ZHANG Tianping, ZHOU Haiyan . Application Scheme of Ion Electric Propulsion System for Main-Belt Asteroid Sample and Return Mission[J]. Journal of Deep Space Exploration, 2015 , 2(2) : 168 -173 . DOI: 10.15982/j.issn.2095-7777.2015.02.011

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