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HIGH-RESOLUTION OPTICAL REMOTE SENSING TELESCOPE FOR MICRO-SPACECRAFT

机译:用于微空间工艺的高分辨率光学遥感望远镜

摘要

The invention relates to optics and space technology, and more particularly to electron optical remote sensing telescopes suitable for use on micro-spacecraft. An optical telescope comprises an optical arrangement of a mirror-lens axial lens with a non-circular aperture, said arrangement including a converging input lens, a primary concave mirror-lens, a secondary convex mirror, and a prefocal two-lens corrector. The secondary convex mirror is situated directly at the centre of the input lens so that the image plane is located close to the rear surface of a fastening system of the primary mirror. The prefocal two-lens corrector is situated at the centre of the primary mirror-lens. Internal shades are mounted in the primary mirror-lens and the secondary mirror. The optical telescope further comprises an optomechanical structure consisting of side posts, a frame, and, mounted on said frame, a holder of the primary mirror-lens, the prefocal two-lens corrector and the shade of the primary mirror-lens. The prefocal two-lens corrector is situated inside the holder. The primary mirror-lens and the shade of the primary mirror-lens are fastened to the outside of the holder. An input lens-secondary mirror assembly and a primary mirror-lens-prefocal two-lens corrector assembly are connected by the side posts. At the primary mirror-lens end, the side posts are fastened to the frame. At the input lens end, the side posts are fastened to an input lens holder. The secondary mirror is fastened to the input lens by a holder of the secondary mirror and the shade of the secondary mirror. The optical telescope further comprises a photodetector of an electron sensor, said photodetector being situated directly behind the prefocal corrector in the focus of the optical arrangement, and being fastened to the outer face of the holder of the primary mirror-lens. The invention allows highly detailed imaging of the Earth's surface using an optical telescope located onboard a micro-spacecraft of the CubeSat 16U variety.
机译:本发明涉及光学和太空技术,更具体地说,涉及适用于微型航天器的电子光学遥感望远镜。一种光学望远镜,包括具有非圆形光圈的镜透镜轴向透镜的光学装置,所述装置包括会聚输入透镜,主凹面镜透镜,副凸面镜和预聚焦两透镜校正器。副凸镜直接位于输入透镜的中心,因此像平面位于主镜固定系统的后表面附近。焦前两镜头校正器位于主镜镜头的中央。内部遮光罩安装在主镜和副镜中。该光学望远镜还包括光机械结构,该光机械结构由侧杆,框架以及安装在所述框架上的主镜透镜的支架,预聚焦两镜校正器和主镜透镜的阴影组成。焦前双镜头校正器位于支架内部。主镜透镜和主镜罩的阴影固定在支架的外部。输入透镜-次要镜组件和主镜-镜头-预焦双镜头校正器组件通过侧柱连接。在主镜端,侧柱固定在镜架上。在输入镜头的一端,侧柱固定在输入镜头支架上。副镜通过副镜的支架和副镜的阴影固定在输入透镜上。光学望远镜还包括电子传感器的光电探测器,所述光电探测器在光学装置的焦点处直接位于预聚焦校正器的后面,并固定在主镜透镜支架的外面。本发明允许使用位于CubeSat 16U型微型航天器上的光学望远镜对地球表面进行高度详细的成像。

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