EFFICIENT LUNAR GRAVITY ASSISTS FOR SOLAR ELECTRIC PROPULSION MISSIONS

被引：0

作者：

Landau, Damon ^{[1
]}

McElrath, Tim P. ^{[1
]}

Grebow, Dan ^{[1
]}

Strange, Nathan J. ^{[1
]}

机构：

[1] CALTECH, Jet Prop Lab, Pasadena, CA 91125 USA

来源：

SPACEFLIGHT MECHANICS 2012 | 2012年 / 143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：

The combination of lunar gravity assists for Earth escape and similar to 1.25 yr. of SEP V-infinity leveraging effectively boosts the performance of a given launch vehicle. Two methods are available to establish a launch period with lunar gravity assists, where the energy achievable with lunar escape has been characterized as a function of right ascension, declination, and launch energy. The increased launch efficiency makes a Falcon 9 perform like an Atlas V (401) at low C-3 or like an Atlas V (531) at high C-3. An Atlas V (551) outperforms a Delta IV Heavy for C-3 above 24 km(2)/s(2).

引用

页码：917 / 934

页数：18

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