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Characteristics of space mini passive hydrogen maser in Shanghai astronomical observatory

机译:上海市天文天文台空间迷你无源氢气的特点

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Shanghai Astronomical Observatory is developing space mini passive hydrogen maser for future application in satellite navigation system. Study on key technologies, including miniatured cavity-bulb assembly, absorption pump and magnetic state selection system, have been carried out. Weight of physical package is controlled within 10kg and atomic signal is up to 2dB. Miniatured electronic package weight of 5Kg is developed while keeping system framework as conventional time-separated control method. Engineering model weighting 14.5Kg has been developed. Frequency stability of 1.2×10-12t-1/2(1s ≤ t ≤ 10000s) and temperature coefficient of 5×10-14/°C are measured. Engineering modification and environmental test are carried out.
机译:上海天文天文台正在开发空间迷你无源氢气扫地机,可将来在卫星导航系统中的应用。已经进行了关键技术研究,包括迷你腔灯泡组件,吸收泵和磁性状态选择系统。物理包的重量在10kg内控制,原子信号高达2dB。在将系统框架保持为传统的时间分离的控制方法的同时,开发了5kg的缩小电子封装重量。开发了工程模型加权14.5kg。 1.2×10 -12 t -1/2 (1s≤t≤10000s)和5×10 -14 -14 的温度系数的频率稳定性/°C测量。进行工程改造和环境测试。

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