SAE AIR 5006/2-1996
固体火箭助推器可靠性指南.第二卷的固体火箭助推器的概率设计和分析方法

Solid Rocket Booster Reliability Guidebook - Volume II Probabilistic Design and Analysis Methods for Solid Rocket Boosters

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标准号

SAE AIR 5006/2-1996

发布日期

1996年06月01日

实施日期

废止日期

无

中国标准分类号

V72

国际标准分类号

49.050

发布单位

美国机动车工程师协会

适用范围

The authors of this guidebook and the solid propulsion industry at large have long been troubled by an inability to absolute demonstrate SRB reliability because, under classic reliability theory, large numbers of tests are required to establish statistically significant reliability values. 240 tests with no failures, for instance, are required to demonstrate 0.99 reliability to a 90% confidence level if a binomial model is used. Since the testing cost for hundreds of large motors like space shuttle SRBs would be prohibitive, the solids industry has always been confronted with a vexing dilemma: (1) what is the fewest number of SRBs that can be tested to establish reliability with high confidence level for commitment to flight and (2) what should the reliability that was established with fewer-than- classical numbers of tests be called (it obviously is not demonstrated reliability in the strictest sense of the definition)?

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