Survey of Moderate-Power Electric Propulsion Systems

被引：11

作者：

Petro, Elaine M. ^{[1
]}

Sedwick, Raymond J. ^{[1
]}

机构：

[1] Univ Maryland, Dept Aerosp Engn, 3179 Martin Hall, College Pk, MD 20742 USA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 2017年 / 54卷 / 03期

基金：

美国国家科学基金会;

关键词：

DISCOVERY-CLASS MISSIONS; HALL THRUSTER; ION THRUSTERS; PERFORMANCE; SPACECRAFT; EXPLORER; ENGINES; MODEL;

D O I：

10.2514/1.A33647

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A survey analyzes electrostatic and electromagnetic thrusters suitable for moderate-power solar electric propulsion (SEP) and radioisotope electric propulsion (REP) exploration missions. Electrothermal thrusters are not included in this survey as they typically have significantly lower Isp, higher thrust, and different intended propulsive applications. For this survey, thrusters have been selected that operate between 0.1 and 10kW, offer an Isp on the order of 1000 s, and thrust levels on the order of mN. The systems that meet these requirements are ion engines, Hall thrusters, and spinoff designs of the two.

引用

页码：529 / 541

页数：13

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