350 rub
Journal Science Intensive Technologies №3 for 2015 г.
Article in number:
Reliability space systems
Authors:
V.E. Patraev - Dr. Sc. (Eng.), Associate Professor, Leading Engineer, JSC «Academician M.F. Reshetnev «Information Satellite Systems» (Zheleznogorsk). Е-mail: Patraev@iss-rechetnev.ru
Yu.V. Maksimov - Deputy General Director, JSC «Academician M.F. Reshetnev «Information Satellite Systems» (Zheleznogorsk)
E.A. Shangina - Post-graduate Student, Design Engineer, JSC «Academician M.F. Reshetnev «Information Satellite Systems» (Zheleznogorsk). Е-mail: shangina@iss-rechetnev.ru
Abstract:
In the article «Reliability space systems» addresses important issues of reliability space systems and provides a possible model for the experimental assessment of the reliability of space systems and components.
Reliability and space complex (CC) is an important performance characteristic and integral internal property of CC, which is structurally laid out in the design stages. The basic optimized requirements for the reliability of these components for future space complex as orbital constellation of spacecraft, ground control, missile and space complex, rocket space assignment spacecraft.
Developed analytical structural diagram reliability and space complex and the proposed model estimates the required reliability, taking into account the performance and the launch of a significant number of CC and SC development JSC «ISS». Proposed evaluation of such a major indicator of the reliability of CC as the availability CC. As the source data can be used indicators of readiness or failure of component parts of the CC or the recovery time of the main elements of the spacecraft, including satellites.
The proposed model estimates of reliability CC applied to the design of advanced CC spacecraft for various purposes.
Pages: 9-13
References
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