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Optical design and intensity interferometry simulations in support of the Kilometer Space Telescope

机译:用于支撑公里望远镜的光学设计和强度干涉测量模拟

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摘要

Very large telescopes will be needed for the future of space science, space laser-com, and other interstellar or interplanetary applications. However, as telescopes' diameters increase, their weight and cost increase dramatically. An approximation for ground-based observatories is that their cost increases to the power of 2.7 of its diameter [SAO, Special Report #385 (1979), p. 9]. Large space-based telescopes become limited by the rocket size and power. Multiple telescopes are also needed for very long baseline interferometry (VLBI), which further increases cost. A solution to overcome these issues is the use of inflatable telescopes. A thin mirror material clearly has much lower mass; however, controlling its surface error or wavefront can be a challenge. Intensity interferometry is an imaging method that has a much looser sensitivity to wavefront error (WFE), and thus is an ideal match for very large inflatable telescopes. A spherical inflatable mirror is the most practical; however, it suffers from spherical aberration. This paper presents new optical designs and simulations for intensity interferometry in support of large inflatable spherical telescopes. The optical system design includes a novel five-mirror off-axis, free-form, spherical aberration corrector. The system design shown is a 10 m diameter f/1 spherical primary mirror with 1.2 arcmin (0.02 degrees) field of view (FOV). MATLAB simulations of intensity interferometry combine signal with noise and WFE. Visibility-based VLBI image simulations are shown based on various telescope arrays. Simulations show that with a 1 GHz detector, a 1 cm RMS WFE is tolerable. So the challenge of the optical design is then more about gathering and concentrating the light down to a reasonable size detector. Further simulations of signal combined with noise indicate that the signal rate must be about 100 times higher than the noise rate for an adequate intensity interferometry measurement. Visibility-based image simulations reveal that many telescopes (5-20 per axis) are needed in a 2D array out to the first visibility minimum to adequately resolve unknown features of a distant object. (C) 2021 Optical Society of America
机译:未来的空间科学、空间激光通信和其他星际或行星际应用将需要非常大的望远镜。然而,随着望远镜直径的增加,它们的重量和成本急剧增加。地面天文台的一个近似值是,它们的成本增加到其直径的2.7倍[SAO,特别报告#385(1979),第9页]。大型天基望远镜受到火箭尺寸和功率的限制。超长基线干涉测量(VLBI)也需要多台望远镜,这进一步增加了成本。解决这些问题的办法是使用充气望远镜。薄镜材料的质量明显要低得多;然而,控制其表面误差或波前可能是一个挑战。强度干涉法是一种成像方法,它对波前误差(WFE)的灵敏度要低得多,因此是非常大的充气望远镜的理想匹配方法。球形充气镜是最实用的;然而,它受到球差的影响。本文介绍了支持大型充气球形望远镜的强度干涉测量的新光学设计和模拟。光学系统设计包括一种新型五镜离轴自由球面像差校正器。所示系统设计为直径10米的f/1球面主镜,视场为1.2弧度(0.02度)。强度干涉测量的MATLAB仿真结合了信号、噪声和WFE。基于可视性的VLBI图像模拟显示了基于各种望远镜阵列。仿真表明,使用1GHz探测器时,1cm RMS WFE是可以接受的。因此,光学设计的挑战更多的是将光收集并集中到一个合理大小的探测器上。对信号和噪声的进一步模拟表明,信号速率必须比噪声速率高约100倍,才能进行适当的强度干涉测量。基于可见度的图像模拟显示,2D阵列中需要许多望远镜(每个轴5-20个),以达到第一个最小可见度,从而充分解析远处物体的未知特征。(2021)美国光学学会

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  • 来源
    《Applied optics》 |2021年第12期|共10页
  • 作者

    Johnson Tim P.; Crowe Devon G.;

  • 作者单位

    Raytheon Technol 2000 E El Segundo Blvd El Segundo CA 90245 USA;

    Arizona Aerosp LLC Tucson AZ 85747 USA;

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  • 正文语种 eng
  • 中图分类 应用;
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