Mission Enabling and Enhancing Spacecraft Capabilities with MicroNewton Electric Propulsion

被引:0
|
作者
Marrese-Reading, Colleen M. [1 ]
Ziemer, John K. [1 ]
Scharf, Daniel P. [1 ]
Martin-Mur, Tomas J. [1 ]
Thompson, Paul [1 ]
Mueller, Juergen [1 ]
Wirz, Richard [2 ]
机构
[1] Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
[2] Univ Calif Los Angeles, Mech & Aerosp Engn Dept, Los Angeles, CA USA
基金
美国国家航空航天局;
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D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The capability to significantly improve current spacecraft pointing, precision orbit maintenance and disturbance mitigation were considered using precision, quiescent microNewton electric propulsion systems. 1,2 The results of the analyses showed that electric propulsion systems operating in the microNewton to hundreds of microNewtons thrust range can offer significant improvements over state-of-the-art mission capabilities to enable 30 m Earth-fixed orbital tubes, constellation spacecraft position control to within nanometers and exoplanet observatory pointing with 0.1 milliarcsecond precision. Electric propulsion thrust characteristics required to support these capabilities are discussed.
引用
收藏
页数:10
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