LUNAR L1 EARTH-MOON PROPELLANT DEPOT ORBITAL AND TRANSFER OPTIONS ANALYSIS

被引:0
作者
Wan, Hsuan-chen [1 ]
Villac, Benjamin F. [1 ]
机构
[1] Univ Calif Irvine, Mech & Aerosp Engn Dept, 4200 Engn Gateway, Irvine, CA 92697 USA
来源
ASTRODYNAMICS 2013, PTS I-III | 2014年 / 150卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
One concept in support of human exploration beyond low Earth orbit consists of placing fuel depots in the region of the Earth-Moon or Earth-Moon-Sun libration points. While several studies have considered this concept on halo orbits, the full range of libration point orbits has not been considered. This study further explores the broader range of quasi-periodic orbits near the LL1 point, and their associated set of transfers from the lunar surface and low lunar orbits.
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页码:2711 / 2725
页数:15
相关论文
共 5 条
  • [1] Hill K., 2006, AIA A/AAS Astrodynamics Specialist Conference and Exhibit, P21
  • [2] Howell Kathleen C., 2010, AAS10120
  • [3] Leaving the Moon by means of invariant manifolds of libration point orbits
    Maria Alessi, Elisa
    Gomez, Gerard
    Masdemont, Josep J.
    [J]. COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2009, 14 (12) : 4153 - 4167
  • [4] Olikara Z. P., 2011, P 7 EUROMECH NONL DY
  • [5] Zegler F., 2010, AIAA SPACE 2010, P8638