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电分离连接器对小卫星星箭分离干扰分析

秦远田 陈卫东

航天器环境工程2012,Vol.29Issue(3):292-296,5.
航天器环境工程2012,Vol.29Issue(3):292-296,5.DOI:10.3969/j.issn.1673-1379.2012.03.011

电分离连接器对小卫星星箭分离干扰分析

Analysis of satellite-rocket separation interfered by the electromagnetic-separation-electric-connector

秦远田 1陈卫东1

作者信息

  • 1. 南京航空航天大学微小卫星研究中心,南京210016
  • 折叠

摘要

Abstract

The successful separation of the Electromagnetic-Separation-Electric-Connector(ESEC) is an important prerequisite for the satellite-rocket separation. In this paper, some microsatellite is considered, whose ESEC has two kinds of separation modes: electric separation and mechanical separation. The separation time sequences in the normal and the abnormal separation modes are analyzed. Two mechanical models in the two separation modes are established. The interference with the satellite separation attitude by the mechanical separation force of the ESEC is simulated. The satellite separation attitude in the abnormal mode is compared with that in the normal mode.

关键词

卫星/星箭分离/电分离连接器/分离姿态

Key words

satellite/satellite-rocket separation/electromagnetic-separation-electric-connector(ESEC)/separation attitude

分类

数理科学

引用本文复制引用

秦远田,陈卫东..电分离连接器对小卫星星箭分离干扰分析[J].航天器环境工程,2012,29(3):292-296,5.

基金项目

南京航空航天大学航天专项 ()

航天器环境工程

OACSTPCD

1673-1379

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