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Minimum flight time and feasibility of multiple orbit transfers between Earth and Mars and between Earth and Venus

机译：地球和火星之间以及地球和金星之间多次轨道转移的最短飞行时间和可行性

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作者
Henry, E. W.;
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年度 1969
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
EARTH-MARS TRAJECTORIES; EARTH-VENUS TRAJECTORIES; FLIGHT TIME; INTERPLANETARY TRANSFER ORBITS; FEASIBILITY ANALYSIS; INTERPLANETARY FLIGHT;

机译：EaRTH-maRs TRaJECTORIEs; EaRTH-VENUs TRaJECTORIEs;飞行时间;行星际转移轨道;可行性分析; INTERpLaNETaRY FLIGHT;
入库时间 2022-08-29 11:14:39

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1. Minimum-Time Trajectory Optimization of Multiple Revolution Low-Thrust Earth-Orbit Transfers [J] . Graham Kathryn F., Rao Anil V. Journal of Spacecraft and Rockets . 2015,第3期

机译：多次旋转低推力地球轨道转移的最小时间轨迹优化
2. Minimum-Time Trajectory Optimization of Low-Thrust Earth-Orbit Transfers with Eclipsing [J] . Graham Kathryn F., Rao Anil V. Journal of Spacecraft and Rockets . 2016,第2期

机译：带推力的低推力地球轨道转移的最小时间轨迹优化
3. Minimum-time Earth-Moon and Moon-Earth orbital maneuvers using time-domain finite element method [J] . S.A. Fazelzadeh, G.A. Varzandian Acta astronautica . 2010,第3a4期

机译：使用时域有限元方法的最小时间地月和月地球轨道机动
4. Minimum-Time Earth-to-Mars Interplanetary Orbit Transfer Assuming Elliptic Planetary Motion [C] . Brittanny V. Holden, Shan He, Anil V. Rao AIAA SciTech Forum and Exposition . 2021

机译：假设椭圆行星运动的最小时间地球到火星行星际轨道转移
5. Classification of Time-Optimal Constant-Acceleration Earth-Mars Transfers. [D] . Campbell, Jesse A. 2014

机译：时间最优恒加速度地球-火星传输的分类。
6. Venus-Earth-Mars: Comparative Climatology and the Search for Life in the Solar System [O] . Roger D. Launius 2012

机译：金星-地球-火星：比较气候学和太阳系中的生命搜寻
7. Memoir of the secular variations of the elements of the orbits of the eight principal planets, Mercury, Venus, the Earth, Mars, Jupiter, Saturn, Uranus, and Neptune; with tables of the same; together with the obliquinity of the ecliptic, and the precession of the equinoxes in both longitude and By John N. Stockwell. [O] . John N. Stockwell 1872

机译：八位主要行星，汞，金星，地球，火星，木星，土星，天王星和海王星和海王星的轨道的世俗变化的回忆录;表格相同;与蒙太基的倾斜度以及经度和约翰斯托克普通的昼夜平分症的动力。
8. Determination of the Minimum Delta V Transfer Trajectory from a Low Earth Orbit to a Stable Orbit Around the Lagrangian Point L4 in a Restricted Four-Body System [R] . Weimer, T. E. 1979

机译：在限制四体系统中确定拉格朗日点L4周围低地球轨道到稳定轨道的最小ΔV传递轨迹

Minimum flight time and feasibility of multiple orbit transfers between Earth and Mars and between Earth and Venus

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