The space interferometer siderostats

B. Jau, M. Badescu, R. Goullioud, B. Trease, Z. Chang, J. Carson, D. Braun, B. Cook
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Abstract

The paper describes the Siderostats (SID) of the Space Interferometry Mission (SIM) that is being developed at JPL. The description focuses on the generic design for the SIDs, having a 336 mm diameter mirror with a double corner cube at the mirror's vertex. Mirror positioning is controlled by single stage linear actuators (no fine stage). The mirror's 8° dual axis tip/tilt rotation is enabled through sets of hexfoil flexures. The entire SID configuration is described, key requirements listed, and results from preliminary analyses mentioned. Design details, positioning and sensing capabilities, as well as results from an actuator life test, are presented.
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这个空间干涉仪是侧移的
本文介绍了喷气推进实验室正在研制的空间干涉测量任务(SIM) Siderostats (SID)。描述的重点是SIDs的通用设计,有一个直径336毫米的镜子,镜子的顶点有一个双角立方体。镜面定位由单级线性执行机构控制(无精细级)。镜子的8°双轴尖端/倾斜旋转是通过一组六边形弯曲来实现的。本文描述了整个SID配置,列出了关键需求,并提到了初步分析的结果。介绍了设计细节、定位和传感能力以及执行器寿命测试的结果。
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