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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。
A tooling design method for mechanical environment test of satellite electric propulsion system was studied. The tooling structure modeling, structural strength and test load analysis and structure optimization design based on simulation results were studied. The rationality of the design.