Reliability apportionment for complex Launch Vehicles

被引：0
|
作者：
Santhamma, K [1 ]
Seenaiah, K [1 ]
机构：
[1] Vikram Sarabhai Space Ctr, Qual Div Mech Syst, Trivandrum 695022, Kerala, India
来源：
SPACE SAFETY, RESCUE AND QUALITY 1999-2000 | 2001年 / 102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：
A methodology is described for obtaining the reliability requirement / goal for each subsystem / component of a Launch Vehicle from its Mission reliability goal. An algorithm has been developed to allocate the mission reliability goal to its various subsystems / components taking into account certain factors which can differentiate among the subsystems, These requirements will directly influence the development cost, test plans for subsystems and schedule.
引用
收藏
页码：93 / 100
页数：8
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