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Reliability evaluation of communication satellite thruster

  • Xiao Fang Mao*
  • , Xiao Rui Yue
  • , Hui Min Fu
  • *此作品的通讯作者
  • Beihang University
  • CAS - Beijing Institute of Control Engineering

科研成果: 期刊稿件文章同行评审

摘要

A reliability evaluation and life prediction method on communication satellite thruster was established for its characters of long life, high manufacturing cost and experimental expense, and most of the obtained data are zero-failure data or very few failure data. For the difficulty to evaluate the reliability of satellite thrusters, a converting principle of information among different test conditions was provided, and successfully solved this problem. Based on these approaches, the reliability of communication satellite thruster can be evaluated with high precision. Data from impulse test and steady test of a thruster were analyzed, and the reliability evaluation for its geostationary orbit and transfer orbit were derived.

源语言英语
页(从-至)2475-2479
页数5
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
26
11
出版状态已出版 - 11月 2011

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