TY - JOUR
T1 - Reliability validation on spacecraft pyrotechnical devices using the hardened test method
AU - Rong, Ji Li
AU - Zhang, Tao
PY - 2009/11
Y1 - 2009/11
N2 - 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.
AB - 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.
KW - Hardened test
KW - Reliability validation
KW - Spacecraft pyrotechnical devices
KW - Strength-stress model
UR - http://www.scopus.com/inward/record.url?scp=72449168403&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2009.06.061
DO - 10.3873/j.issn.1000-1328.2009.06.061
M3 - Article
AN - SCOPUS:72449168403
SN - 1000-1328
VL - 30
SP - 2426
EP - 2430
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 6
ER -