Reliability evaluation of communication satellite thruster

  • Xiao Fang Mao*
  • , Xiao Rui Yue
  • , Hui Min Fu
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)2475-2479
Number of pages5
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume26
Issue number11
StatePublished - Nov 2011

Keywords

  • Communication satellite thruster
  • Geostationary orbit
  • Reliability evaluation
  • Transfer orbit
  • Very few failure data
  • Zero failure data

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