Aircraft Engineering
Аuthors
1*, 2**1. ,
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: kafedra_602@mail.ru
**e-mail: v.s.safronov@mail.ru
Abstract
Safety factor influence upon a flight vehicle composite structural elements reliability is studied for forced tests. Analytic relationships between structure part reliability and test weighting coefficient, assurance factor, number of damage-free tests are derived.
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