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卫星太阳电池阵在板展开阶段的撞击特性研究

刘锦阳 洪嘉振

空间科学学报2000,Vol.20Issue(1):61-68,8.
空间科学学报2000,Vol.20Issue(1):61-68,8.

卫星太阳电池阵在板展开阶段的撞击特性研究

CONTACT-IMPACT OF SOLAR BATTERY DURING THE DEPLOYMENT OF THE PLATES

刘锦阳 1洪嘉振1

作者信息

  • 1. 上海交通大学工程力学系 200030
  • 折叠

摘要

Abstract

In this paper, the contact-impact problem of solarbattery during the deployment of plates is studied. The equation ofmotion of flexible multibody system during impact is derived. The timehistories of impact forces and the acceleration of some nodes of theplates are presented. It shows that the impact forces of the contactpoints reach the peak at different time on account of the distortion ofthe flexible plates. It also shows that when impact occurs, theacceleration of the nodes near the impact points are greater than thatof the other nodes, and it takes few time for the impact wave to spreadthrough the flexible plates. When the impact wave reaches the nodes atthe boundary of the outer plate, the acceleration of the nodes becomesgreater and vibrant which leads to the swinging of the plates.

关键词

卫星太阳电池阵—撞击力—扭转

Key words

Solar battery/Impact force/Distortion

分类

航空航天

引用本文复制引用

刘锦阳,洪嘉振..卫星太阳电池阵在板展开阶段的撞击特性研究[J].空间科学学报,2000,20(1):61-68,8.

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