AN ATTITUDE CONTROL SYSTEM FOR LARGE LAUNCH VEHICLES

被引：1
|
作者：
SELTZER, SM
机构：
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1969年 / 6卷 / 06期
关键词：
D O I：
10.2514/3.29653
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：748 / +
页数：1
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