| 卫星电推进系统力学环境试验工装设计 |
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| 引用本文： | 黄佳婕,卫佳,廖云龙.卫星电推进系统力学环境试验工装设计[J].火箭推进,2013,39(1):72-76. |
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| 作者姓名： | 黄佳婕 卫佳 廖云龙 |
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| 作者单位： | 上海空间推进研究所,上海,201112 |
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| 基金项目： | 中国航天科技集团公司支撑项目(2007JY06) |
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| 摘 要： | 研究了一种卫星电推进系统进行力学环境试验的工装设计方法,进行了工装结构建模、结构强度与试验载荷的分析以及建立在仿真计算结果上的结构优化设计,并通过试验验证了该项设计的合理性。
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| 关 键 词： | 工装结构设计 力学环境试验 仿真计算 优化设计 |
Design of technological rig for mechanical environment test for satellite electric propulsion system |
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| HUANG Jia-jie
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WEI Jia
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LIAO Yun-long.Design of technological rig for mechanical environment test for satellite electric propulsion system[J].Journal of Rocket Propulsion,2013,39(1):72-76. |
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| Authors: | HUANG Jia-jie WEI Jia LIAO Yun-long |
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| Institution: | (Shanghai Institute of Space Propulsion,Shanghai 201112,China) |
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| Abstract: | A design method of technological rig for mechanical environment test of a satellite electric propulsion system is introduced. The technological rig modeling, structural strength and test load analyses, and structural optimal design based on simulation results were carried out. The effectiveness of the method was validated by experiment. |
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| Keywords: | structural design of technological rig mechanical environment test simulation calculation optimization design |
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