Approximate solutions for lunar trajectory and vehicle optimization using electric propulsion

被引：0
|
作者：
Kluever, CA [1 ]
Chang, KR [1 ]
机构：
[1] UNIV MISSOURI, DEPT MECH & AEROSP ENGN, KANSAS CITY, MO 64110 USA
来源：
SPACEFLIGHT MECHANICS 1996, PTS 1 AND 2 | 1996年 / 93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：
引用
收藏
页码：3 / 13
页数：11
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