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Development of optical system for the NISS onboard NEXTSat-1

机译:为NISSS-1上的NISS开发光学系统

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Korea Astronomy and Space Science Institute (KASI) successfully developed the Near-infrared Imaging Spectrometer for Star formation history (NISS), which is a scientific payload for the next-generation small satellite-1 (NEXTSat-1) in Korea and is expected to be launched in 2018. The major science cases of NISS are to probe the star formation in local and early Universe through the imaging spectroscopic observations in the near-infrared. The off-axis catadioptric optics with 150mm aperture diameter is designed to cover the FoV of 2×2 deg with the passband of 0.95-2.5μm. The linear variable filter (LVF) is adopted as a disperse element with spectral resolution of R~20. Given the error budgets from the optical tolerance analysis, all spherical and non-spherical surfaces were conventionally polished and finished in the ultra-precision method, respectively. Primary and secondary mirrors were aligned by using interferometer, resulting in residual wave-front errors of P-V 2.7μm and RMS 0.61μm, respectively. To avoid and minimize any misalignment, lenses assembled were confirmed with de-centering measurement tool from Tri-Optics. As one of the key optical design concepts, afocal beam from primary and secondary mirrors combined made much less sensitive the alignment process between mirrors and relay lenses. As the optical performance test, the FWHM of PSF was measured about 16μm at the room temperature, and the IR sensor was successfully aligned in the optimized position at the cryogenic temperature. Finally, wavelength calibration was executed by using monochromatic IR sources. To support the complication of optical configuration, the opto-mechanical structure was optimized to endure the launching condition and the space environment. We confirmed that the optical performance can be maintained after the space environmental test. In this paper, we present the development of optical system of NISS from optical design to performance test and calibration.
机译:韩国天文学和太空科学研究所(KASI)成功开发了用于恒星形成历史(NISS)的近红外成像光谱仪,该光谱仪是韩国下一代小卫星1(NEXTSat-1)的科学有效载荷,有望实现NISS将于2018年发射升空。NISS的主要科学案例是通过近红外光谱成像观测来探测本地和早期宇宙中的恒星形成。孔径为150mm的离轴折反射光学器件设计为通过0.95-2.5μm的通带覆盖2×2度的FoV。采用线性可变滤波器(LVF)作为色散元件,光谱分辨率为R〜20。根据光学容差分析给出的误差预算,所有球形和非球形表面都分别按常规进行了抛光和超精密加工。使用干涉仪对准主镜和副镜,分别导致P-V的残留波前误差为2.7μm和RMS为0.61μm。为了避免并最大程度地减少未对准,已使用Tri-Optics的偏心测量工具确认了已组装的镜片。作为关键的光学设计概念之一,来自主反射镜和辅助反射镜的合焦光束使反射镜和中继透镜之间的对准过程变得不那么敏感。作为光学性能测试,在室温下测得的PSF的FWHM约为16μm,并且在低温下将红外传感器成功地对准了最佳位置。最后,通过使用单色红外光源执行波长校准。为了支持复杂的光学配置,对光机械结构进行了优化,以承受发射条件和空间环境。我们确认,在进行空间环境测试后,可以保持光学性能。在本文中,我们介绍了NISS光学系统从光学设计到性能测试和校准的发展。

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