Reliability validation on spacecraft pyrotechnical devices using the hardened test method

Ji Li Rong*, Tao Zhang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

10 Citations (Scopus)

Abstract

A strength-stress model for the reliability of spacecraft pyrotechnical devices is proposed, based on the mechanical characters of the products and one-shot product reliability assessment theory. From this, a reliability validation method with small sample under hardened conditions was presented. In this method the products are tested under hardened conditions. If they can still work without failure under such conditions, then the reliability in normal conditions can be calculated by a series of formulas. It indicates that using this method, with the confidence level of 0.95, only less than 10 times trials are needed to validate the reliability of 0.9999~0.99999. Finally, the design of test under severe conditions was described.

Original languageEnglish
Pages (from-to)2426-2430
Number of pages5
JournalYuhang Xuebao/Journal of Astronautics
Volume30
Issue number6
DOIs
Publication statusPublished - Nov 2009

Keywords

  • Hardened test
  • Reliability validation
  • Spacecraft pyrotechnical devices
  • Strength-stress model

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