Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test
To determine the missile’s number using in the manufacture finalization firing test to examine the missile’s self-flying reliability. Firstly, the firing test scheme recommended by the consumer is introduced, which is designed under the condition that the maturity goal is tak...
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Editorial Office of Aero Weaponry
2021
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oai:doaj.org-article:291c136465e44823828199d8e06dc3d62021-11-30T00:13:33ZReliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test1673-504810.12132/ISSN.1673-5048.2020.0255https://doaj.org/article/291c136465e44823828199d8e06dc3d62021-08-01T00:00:00Zhttps://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1631769651978-897016107.pdfhttps://doaj.org/toc/1673-5048To determine the missile’s number using in the manufacture finalization firing test to examine the missile’s self-flying reliability. Firstly, the firing test scheme recommended by the consumer is introduced, which is designed under the condition that the maturity goal is taken as the lower test limit, then quantitatively analyzing the probabilities passing the recommended firing test scheme when the missile’s reliability is different. The probability passing the recommended firing test scheme is small even though the missile’s reliability is equal to the maturity goal, the reason is that the maturity goal be wrong taken as the lower test limit. The manufacture finalization firing test scheme should be designed according to the principle which the reliability minimum acceptable value be examined and whether the maturity goal can be reached or not, so that the missile’s number using in the manufacture finalization firing test and the failure number allowed are determined.Li Gencheng, Li HongyuEditorial Office of Aero Weaponryarticle|reliability|manufacture finalization|firing test|maturity goal|minimum acceptable value|lower test limitMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 4, Pp 7-10 (2021) |
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|reliability|manufacture finalization|firing test|maturity goal|minimum acceptable value|lower test limit Motor vehicles. Aeronautics. Astronautics TL1-4050 |
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|reliability|manufacture finalization|firing test|maturity goal|minimum acceptable value|lower test limit Motor vehicles. Aeronautics. Astronautics TL1-4050 Li Gencheng, Li Hongyu Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
description |
To determine the missile’s number using in the manufacture finalization firing test to examine the missile’s self-flying reliability. Firstly, the firing test scheme recommended by the consumer is introduced, which is designed under the condition that the maturity goal is taken as the lower test limit, then quantitatively analyzing the probabilities passing the recommended firing test scheme when the missile’s reliability is different. The probability passing the recommended firing test scheme is small even though the missile’s reliability is equal to the maturity goal, the reason is that the maturity goal be wrong taken as the lower test limit. The manufacture finalization firing test scheme should be designed according to the principle which the reliability minimum acceptable value be examined and whether the maturity goal can be reached or not, so that the missile’s number using in the manufacture finalization firing test and the failure number allowed are determined. |
format |
article |
author |
Li Gencheng, Li Hongyu |
author_facet |
Li Gencheng, Li Hongyu |
author_sort |
Li Gencheng, Li Hongyu |
title |
Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
title_short |
Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
title_full |
Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
title_fullStr |
Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
title_full_unstemmed |
Reliability Analyzing on Missile’s Number Using in Manufacture Finalization Firing Test |
title_sort |
reliability analyzing on missile’s number using in manufacture finalization firing test |
publisher |
Editorial Office of Aero Weaponry |
publishDate |
2021 |
url |
https://doaj.org/article/291c136465e44823828199d8e06dc3d6 |
work_keys_str_mv |
AT ligenchenglihongyu reliabilityanalyzingonmissilex02019snumberusinginmanufacturefinalizationfiringtest |
_version_ |
1718406851996942336 |