Method for Transferring a Spacecraft from Geosynchronous Transfer Orbit to Lunar Orbit

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Method for Transferring a Spacecraft from Geosynchronous Transfer Orbit to Lunar Orbit

机译：将航天器从地球同步转移轨道转移到月球轨道的方法

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This novel innovation from Ames Research Center allows spacecraft to share rides with larger spacecraft that are headed to Geosynchronous Earth Orbit (GEO). The secondary spacecraft is dropped off Geosynchronous Transfer Orbit (GTO) at any time during the day or year, and will subsequently enter lunar orbit, with no constraint on the lunar orbit inclination. The secondary spacecraft can be relatively small, riding as a secondary payload with a larger primary spacecraft. The secondary spacecraft is intended to be controllable (i.e., maneuverable).

机译：艾姆斯研究中心（Ames Research Center）的这项创新技术使航天器可以与前往地球同步地球轨道（GEO）的大型航天器共享飞行。辅助航天器在一天或一年中的任何时候都从地球同步转移轨道（GTO）上落下，随后将进入月球轨道，而对月球轨道的倾斜度没有任何限制。次级航天器可以相对较小，可以与较大的初级航天器一起作为次级有效载荷骑行。辅助航天器旨在是可控制的（即可操纵的）。

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《NASA Tech Briefs》 |2018年第5期|46-46|共1页
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1. Low-Thrust Transfers to Lunar Orbits from Halo Orbits Around Lunar Libration Points L1 and L2 [J] . Shirobokov M. G., Trofimov S. P. Cosmic research . 2020,第3期

机译：从Lunar Libration点L1和L2周围的Halo轨道转移到月球轨道的低推力转移
2. Geosynchronous transfer orbits as a market for impulse delivered by lunar sourced propellant [J] . Bennett Nicholas James, Dempster Andrew G. Planetary and space science . 2020,第Mara期

机译：地球同步转移轨道作为月球源推进剂传递的冲力市场
3. Planar Problem of an Optimal Transfer of a Low-Thrust Spacecraft from High-Elliptic to Geosynchronous Orbit [J] . R. Z. Akhmetshin Cosmic research . 2004,第3期

机译：低推力航天器从高椭圆轨道到地球同步轨道最优转移的平面问题
4. Indirect Optimization of Low Earth Orbit to Low Lunar Orbit Transfers [C] . C. Ranieri, C. Ocampo AIAA guidance, navigation and control conference and exhibit . 2008

机译：低地球轨道到低月球轨道转移的间接优化
5. Analytical theory for orbits of electrostatically charged spacecraft and direct calculation of planet-to-planet transfers [D] . Gangestad, Joseph W. 2010

机译：带静电航天器的轨道分析理论和行星到行星转移的直接计算
6. Charge Transfer Through Single- and Double-strand DNAs: Simulations Based on Molecular Dynamics and Molecular Orbital Methods [O] . Ken-ichi Dedachi, Takayuki Natsume, Taisuke Nakatsu, -1

机译：通过单链和双链DNA的电荷转移：基于分子动力学和分子轨道方法的模拟
7. Solar sailcraft motion in sun-earth-moon space with application to lunar transfer from geosynchronous orbit [O] . Salvail, James Ronald 1991

机译：太阳地球月球空间中的太阳帆船运动应用于地球同步轨道的月球转移
8. Simple Method of Using Onboard Optical Measurements to Predict the Orbit Established after the Lunar-Ascent-Transfer Orbit [R] . Baker, L. K., Fletcher, H. S. 1970

机译：使用板载光学测量来预测月球 - 上升 - 转移轨道后建立的轨道的简单方法

Method for Transferring a Spacecraft from Geosynchronous Transfer Orbit to Lunar Orbit

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