Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors
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Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors
Vol. 26, Issue 4, (2011)
作者机构:
1. 北京航空航天大学 可靠性与系统工程学院,北京,100191
2. 中国运载火箭技术研究院 北京宇航系统工程研究所,北京,100076
作者简介:
基金信息:
DOI:
CLC:
Published:2011
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LI Jin, ZHAO Yu, LI Wen-zhao, et al. Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors[J]. 2011, 26(4).
DOI:
LI Jin, ZHAO Yu, LI Wen-zhao, et al. Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors[J]. 2011, 26(4).DOI:
Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors
The problem of liquid-propellant rocket engine's reliability compliance test plans at present is that ignoring the processes of firing and shutdown or the test taking too long.To solve this problem
considering typical compliance test plans of binomial distribution and Weibull distribution
using the weighting factors
the method of reliability compliance test plan developing was provided.The duration of firing was verified in this reliability compliance test plans developing method
at the same time the processes of firing and shutdowns were also considered.This reliability compliance test plan utilized development information and saved the test time and cost.