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卫星太阳电池阵平展试验的冲击测试与冲击抑制

黄杰 侯鹏 李志慧 尤超蓝

航天器环境工程2018,Vol.35Issue(2):118-122,5.
航天器环境工程2018,Vol.35Issue(2):118-122,5.DOI:10.3969/j.issn.1673-1379.2018.02.003

卫星太阳电池阵平展试验的冲击测试与冲击抑制

Measurement and suppression of impact in horizontal deployment test for satellite solar array

黄杰 1侯鹏 2李志慧 2尤超蓝1

作者信息

  • 1. 上海卫星工程研究所,上海 201109
  • 2. 上海卫星装备研究所,上海 200240
  • 折叠

摘要

Abstract

In order to accurately determine the impact of the satellite solar array in its horizontal development test process, and reduce the negative effects of the impact during the test, a mathematical model is established for simulating the test process. The impact test scheme and the impact inhibition mechanism are designed. As an example, a model test is carried out for a certain satellite's solar array to verify the impact effect during the development process. The results show that the impact suppression mechanism works well with an effective suppression of the acceleration at the hinges.

关键词

卫星/太阳电池阵/水平展开/冲击测试/冲击抑制

Key words

satellite/solar array/horizontal deployment/impact test/impact suppression

分类

航空航天

引用本文复制引用

黄杰,侯鹏,李志慧,尤超蓝..卫星太阳电池阵平展试验的冲击测试与冲击抑制[J].航天器环境工程,2018,35(2):118-122,5.

基金项目

军委专项基金项目(编号:17-163-18-XX-001-054-01) (编号:17-163-18-XX-001-054-01)

航天器环境工程

OACSTPCD

1673-1379

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