Liquid propulsion launch vehicle reliability in closed form

被引：3
|
作者：
Huang, ZF
Weber, TF
机构：
[1] Boeing Co, Rocketdyne Prop & Power, Canoga Park, CA 91309 USA
[2] Boeing Co, Downey, CA 90241 USA
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1999年 / 36卷 / 05期
关键词：
D O I：
10.2514/2.3482
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The derivations of two closed-form formulas for calculating liquid propulsion launch vehicle system reliability are presented, and the formulas with application examples are illustrated. These formulas overcome the inadequacy of some existing formulas and inefficiency of Monte Carlo simulation and serve as an efficient analytical tool for accurate system reliability evaluation under a given set of input parameter conditions. Therefore, they greatly help system-level trade studies and optimization.
引用
收藏
页码：701 / 703
页数：3
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