Title of the article

RELIABILITY MODELING THE THERMAL CONTROL SYSTEM OF SPACECRAFT IN STAGE ELECTRICAL TESTING

Authors

Belova Victoria Victorovna, postgraduate student, engineer‒system tester, Rocket and Space Corporation «Energia» named after S. P. Korolev

Index UDK

629.7.017

Abstract

In the article presents the problem of modeling the reliability for the thermal control system of «Progress » cargo transportation spacecraft. Model is founded on the basis reliability block diagram, phase block diagram, fault tree methodology, implemented in the software package Relex. The simulation results are proposed to use for the program evaluation as a priori failure level reliability of the thermal control system «Progress» cargo transportation spacecraft during electrical testing.

Key words

stage of electrical testing; reliability model; reliability block diagram; phase block diagram; faulttree.

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Дата создания: 31.03.2015 12:29
Дата обновления: 31.03.2015 12:29