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Implementation of the Chicago sum frequency laser at Palomar laser guide star test bed

机译:在Palomar激光导星测试台上实现Chicago sum频率激光器

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Work is underway at the University of Chicago and Caltech Optical Observatories to implement a sodium laser guide star adaptive optics system for the 200 inch Hale telescope at Palomar Observatory. The Chicago sum frequency laser (CSFL) consists of two pulsed, diode-pumped, mode-locked Nd:YAG lasers working at 1.064 micron and 1.32 micron wavelengths. Light from the two laser beams is mixed in a non-linear crystal to produce radiation centered at 589 nm with a spectral width of 1.0 GHz (FWHM) to match that of the Sodium-D2 line. Currently the 1.064 micron and 1.32 micron lasers produce 14 watts and 8 watts of TEM-00 power respectively. The laser runs at 500 Hz rep. rate with 10% duty cycle. This pulse format is similar to that of the MIT-Lincoln labs and allows range gating of unwanted Rayleigh scatter down an angle of 60 degrees to zenith angle. The laser system will be kept in the Coude lab and will be projected up to a laser launch telescope (LLT) bore-sited to the Hale telescope. The beam-transfer optics, which conveys the laser beam from the Coude lab to the LLT, consists of motorized mirrors that are controlled in real time using quad-cell positioning systems. This needs to be done to prevent laser beam wander due to deflections of the telescope while tracking. There is a central computer that monitors the laser beam propagation up to the LLT, the interlocks and safety system status, laser status and actively controls the motorized mirrors. We plan to install a wide-field visible camera (for high flying aircraft) and a narrow field of view (FoV) IR camera (for low-flying aircraft) as part of our aircraft avoidance system.
机译:芝加哥大学和加州理工学院光学天文台正在进行工作,以在帕洛玛天文台为200英寸的黑尔望远镜实施钠激光导星自适应光学系统。芝加哥和频激光器(CSFL)由两个脉冲,二极管泵浦,锁模Nd:YAG激光器组成,工作波长为1.064微米和1.32微米。来自两个激光束的光在非线性晶体中混合以产生以589 nm为中心的辐射,其光谱宽度为1.0 GHz(FWHM)以匹配Sodium-D2线。目前,1.064微米和1.32微米的激光器分别产生14瓦和8瓦的TEM-00功率。激光以500 Hz rep运行。占空比为10%的速率。这种脉冲格式类似于MIT-Lincoln实验室的脉冲格式,并允许将不需要的瑞利散射的范围选通控制在与天顶角成60度角的范围内。激光系统将保存在Coude实验室中,并将投射到位于Hale望远镜膛内的激光发射望远镜(LLT)。光束传输光学系统将激光束从库德实验室传输到LLT,由电动反射镜组成,该反射镜使用四单元定位系统进行实时控制。这样做是为了防止激光束在跟踪时因望远镜的偏转而漂移。有一台中央计算机,可监控直至LLT的激光束传播,联锁装置和安全系统状态,激光状态并主动控制电动后视镜。我们计划在飞机回避系统中安装一个广角可见摄像机(用于高空飞行的飞机)和一个窄视场(FoV)红外摄像机(用于低空飞行的飞机)。

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