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Optical testing of a membrane diffractive optic for space-based solar imaging

机译:用于天基太阳成像的膜衍射光学器件的光学测试

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We describe imaging capabilities of a 0.2 m membrane diffractive primary (DOE) used as a key element in FalconSat-7, a space-based solar telescope. Its mission is to take an image of the Sun at the H-alpha wavelength (656nm) over a narrow bandwidth while in orbit. In this case the DOE is a photon sieve which consists of billions of tiny holes, with the focusing ability dependent on an underlying Fresnel zone geometry. Uniform radial expansion/contraction of the substrate due to temperature or relative humidity change will result in a shift in focal length without introducing errors in phase of the transmitted wavefront and without a decrease in efficiency. We will also show that while ideally the DOE surface should be held flat to within 5.25 microns, an opto-mechanical analysis showed that local deformations up to 32 microns are possible without significantly degrading the image quality.
机译:我们描述了用作天基太阳望远镜FalconSat-7的关键要素的0.2 m膜衍射初级(DOE)的成像能力。它的任务是在轨道上以窄带宽在H-alpha波长(656nm)拍摄太阳图像。在这种情况下,DOE是一个由数十亿个小孔组成的光子筛,其聚焦能力取决于下面的菲涅尔带几何形状。由于温度或相对湿度的变化而导致的基板的均匀径向膨胀/收缩将导致焦距的偏移,而不会引起透射波前的相位误差,并且不会降低效率。我们还将显示,尽管理想情况下,DOE表面应保持平坦至5.25微米以内,但光机械分析表明,在不显着降低图像质量的情况下,最大可达到32微米的局部变形。

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