OPTIMUM DESIGN PARAMETERS FOR A SPIN-STABILIZED SPACECRAFT NUTATION DAMPER

被引：1

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作者：

CLOUTIER, GJ

机构：

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1972年 / 9卷 / 06期

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D O I：

10.2514/3.61715

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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页码：466 / &

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