Electric solar wind sail mass budget model

被引:70
作者
Janhunen, P. [1 ]
Quarta, A. A. [2 ]
Mengali, G. [2 ]
机构
[1] Finnish Meteorol Inst, FIN-00101 Helsinki, Finland
[2] Univ Pisa, Dept Civil & Ind Engn, Pisa, Italy
基金
芬兰科学院;
关键词
25;
D O I
10.5194/gi-2-85-2013
中图分类号
P [天文学、地球科学];
学科分类号
07 ;
摘要
The electric solar wind sail (E-sail) is a new type of propellantless propulsion system for Solar System transportation, which uses the natural solar wind to produce spacecraft propulsion. The E-sail consists of thin centrifugally stretched tethers that are kept charged by an onboard electron gun and, as such, experience Coulomb drag through the high-speed solar wind plasma stream. This paper discusses a mass breakdown and a performance model for an E-sail spacecraft that hosts a mission-specific payload of prescribed mass. In particular, the model is able to estimate the total spacecraft mass and its propulsive acceleration as a function of various design parameters such as the number of tethers and their length. A number of subsystem masses are calculated assuming existing or near-term E-sail technology. In light of the obtained performance estimates, an Esail represents a promising propulsion system for a variety of transportation needs in the Solar System.
引用
收藏
页码:85 / 95
页数:11
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