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The lifetime of a lunar satellite orbit is constrained by the non-spherical nature of the Moon’s gravity field. The orbital lifetime of lunar orbits depends significantly on the initial conditions of the orbit. Right ascension of ascending node (Ω) is one of the important orbital parameter affecting the orbital lifetime. In the present work we have analyzed the effect of Ω on the variation of lifetime with altitude for circular lunar orbits. It is found that at a particular initial altitude, a small increase in the altitude results in substantial increase in the orbital lifetime due to effect of the long periodic terms of Earth’s gravity on eccentricity and this transition altitude is different for different Ω. Further, it is observed that the variation of transition altitude with Ω follows a definite, but different trend for orbits with different inclinations. The transition altitude for polar orbits is found to be higher without the effect of Sun and Earth gravity. Variation of transition altitude with orbital inclination is also analyzed. Lifetimes of high altitude circular lunar orbits are analyzed and it is observed that at high altitudes lifetime decreases with altitude.
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篇名 Effect of Altitude, Right Ascension of Ascending Node and Inclination on Lifetime of Circular Lunar Orbits
来源期刊 天文学与天体物理学国际期刊(英文) 学科 医学
关键词 LIFETIME of LUNAR ORBITS Transition ALTITUDE Right Ascension of Ascending NODE Polar ORBITS Long-Periodic Effects of Earth’s Gravity
年,卷(期) 2011,(3) 所属期刊栏目
研究方向 页码范围 155-163
页数 9页 分类号 R73
字数 语种
DOI
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节点文献
LIFETIME
of
LUNAR
ORBITS
Transition
ALTITUDE
Right
Ascension
of
Ascending
NODE
Polar
ORBITS
Long-Periodic
Effects
of
Earth’s
Gravity
研究起点
研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
天文学与天体物理学国际期刊(英文)
季刊
2161-4717
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
333
总下载数(次)
0
总被引数(次)
0
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