Delta-v requirements for earth co-orbital rendezvous missions

被引:17
|
作者
Stacey, R. Greg [1 ,2 ]
Connors, Martin [2 ]
机构
[1] Univ Alberta, Edmonton, AB T6G 2E1, Canada
[2] Athabasca Univ, Athabasca, AB T9S 3A3, Canada
关键词
Asteroid; Rendezvous; Co-orbital; Quasi-satellite; Earth; QUASI-SATELLITE; SOLAR-SYSTEM; DISCOVERY; STABILITY;
D O I
10.1016/j.pss.2009.01.013
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Earth co-orbital asteroids present advantages as potential targets for future asteroid rendezvous missions. Their prolonged proximity to Earth facilitates communication, while their Earth-like orbits mean a steady flux of solar power and no significant periodic heating and cooling of the spacecraft throughout the course of the mission. Theoretical studies show that low-inclination co-orbital orbits are more stable than high-inclination orbits. As inclination is the most significant indicator of low delta-v rendezvous orbits, there is the potential for a large population of easily accessible asteroids, with favorable engineering requirements. This study first looks at phase-independent rendezvous orbits to a large number of objects, then looks in more detail at the phase-dependent orbits to the most favorable objects. While rendezvous orbits to co-orbital objects do not have a low delta-v necessarily, some objects present energy requirements significantly less than previous rendezvous missions. Currently we find no ideal co-orbital asteroids for rendezvous missions, although theoretical Earth Trojans present very low-energy requirements for rendezvous. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:822 / 829
页数:8
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