首页 | 本学科首页   官方微博 | 高级检索  
     

射频电缆低温扭转阻力矩对卫星展开锁定机构的影响
引用本文:黄业平,范凯,蒋国伟. 射频电缆低温扭转阻力矩对卫星展开锁定机构的影响[J]. 航天器环境工程, 2013, 30(3): 245-249
作者姓名:黄业平  范凯  蒋国伟
作者单位:1.上海卫星工程研究所, 上海 200240
摘    要:
针对射频电缆在低温环境下扭转阻力矩增大给某卫星展开锁定机构可靠性带来的不确定影响,文章首先对射频电缆低温扭转阻力矩进行测试试验,之后分析了该阻力矩对展开锁定机构静力矩裕度的影响;在此基础上对机构的设计方案进行改进,并通过仿真分析,验证了改进后机构能够可靠展开,展开时间、冲击力矩等指标满足卫星总体要求。

关 键 词:射频电缆   扭转阻力矩   展开锁定机构   低温试验

Influence of RF cable's low-temperature resistance torque on the deployable and lockable mechanism for satellite
Huang Yeping,Fan Kai and Jiang Guowei. Influence of RF cable's low-temperature resistance torque on the deployable and lockable mechanism for satellite[J]. Spacecraft Environment Engineering, 2013, 30(3): 245-249
Authors:Huang Yeping  Fan Kai  Jiang Guowei
Affiliation:1.Shanghai Institute of Satellite Engineering, Shanghai 200240, China
Abstract:
Based on the effect of the RF cable’s low-temperature resistance torque on the deployable and lockable mechanism for a satellite,a test of the RF cable’s resistance torque at low temperature is carried out.The effect of the resistance torque on the static torque budget of the deployable and lockable mechanism is analyzed.On the basis of the torque analysis,an improved design scheme of the mechanism is proposed,and the simulation analysis is conducted for the scheme.It is shown that the improved mechanism can be deployed reliably,and the parameters,including its deployment time,the impact torque,and others,can meet the general requirements of the satellite system design.
Keywords:RF cable  resistance torque  deployable and lockable mechanism  low-temperature test
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《航天器环境工程》浏览原始摘要信息
点击此处可从《航天器环境工程》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号