| 星载有效载荷印制插件板的力学设计 |
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| 引用本文： | 岑寅昌,宋之玉.星载有效载荷印制插件板的力学设计[J].上海航天,1996(4):33-36. |
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| 作者姓名： | 岑寅昌 宋之玉 |
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| 作者单位： | 航天工业总公司８５１１所 |
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| 摘 要： | 根据星载有效载荷的工作环境及其印刷插件板的设计形式，对有／无加强筋的印制插件权分别用空间飞行器结构有限元分析程序（ＥＤＡＳＳ）进行仿真试验和力学分析，同时也进行了实物振动试验。最后对两种试验的结果进行了比较。
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| 关 键 词： | 星载有效载荷，~＋印制插件板，~＋力学仿真，振动试验 |
MECHANICS DESIGN OF PRINTED CARD AS SATELLITE-ABORD PLAYLOAD |
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| Cen Yinchang,Song Zhiyu,Ren Hanneng.MECHANICS DESIGN OF PRINTED CARD AS SATELLITE-ABORD PLAYLOAD[J].Aerospace Shanghai,1996(4):33-36. |
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| Authors: | Cen Yinchang Song Zhiyu Ren Hanneng |
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| Institution: | No.8511 Institute of Aerospace Industrial Corp. |
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| Abstract: | ayloads are the some of functional the in satellited or spacectafts;they are used to complete tasks,such as predetermined scientific detection,communication, radio recommaissance,biochemical test and special process,and so on.The configurations of these devices are mainly integrated units of printed cards except some devices(for biochemics,optics and process),the reliability of mechanics design effects directly the completion of scientific tasks.This paper presents general designs of the printed cards and the.results of mechanics analysis, giving a reference to person of the same trade or occupation. |
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