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Designs of a miniaturized sapphire-loaded cavity for space borne hydrogen masers

机译:用于空间载氢粉碎机的小型化蓝宝石装载腔的设计

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The previous compact hydrogen maser with sapphire microwave cavity in the Beijing Institute of Radio Metrology and Measurement is not suitable for a space application in navigation systems since a bit large volume and weight. In order to reduce the total size of hydrogen maser atomic clocks further, in this work, the authors have performed the detailed analysis and some theoretical and experimental result in optimizing parameters in a TE011 mode sapphire-loaded cavity resonator more suitable for space borne hydrogen maser. The minimization of the total cavity volume and maximization of the quality factor are both sought finally. Methods of theoretical calculations, finite element simulation, and related experiments have been performed in the process of designing a sapphire loaded cavity. Based on the analysis, a miniaturized sapphire microwave cavity with the total volume of 3.04 dm3, the quality factor 67500, and frequency-temperature coefficient - 59.7 kHz/square is developed. The experimental results are completely consistent with modeled values. In addition, the theoretical calculation result shows that the product of the z-component of the magnetic energy filling factor in the bulb region and the cavity TE_(011) mode Q-factor is 4.08E4 at 50 square in the designed miniaturized sapphire cavity. In addition, two sapphire loaded cavities in the NICT, Japan and in IRCOM, France are detailedly compared with that of our designs.
机译:以前的紧凑型氢气发射机与蓝宝石微波腔内北京无线电计量研究所和测量不适用于航行系统中的空间应用,因为有点大的体积和重量。为了进一步降低氢气发射原子钟的总大小,在这项工作中,作者进行了详细的分析和一些理论和实验结果,优化了TE011模式中的参数蓝宝石装载的腔谐振器更适合空间载氢气升降机。最后,最小化总腔体积和最大化质量因子的最大化均始终寻求。理论计算方法,有限元模拟和相关实验已经在设计蓝宝石装载腔的过程中进行。基于分析,开发了一种小型化的蓝宝石微波腔,具有3.04dm3,质量因子67500和频率温度系数 - 59.7 kHz /平方。实验结果与建模值完全一致。此外,理论计算结果表明,在灯泡区域和腔TE_(011)模式Q-系数中的磁能填充因子的Z组分的乘积为4.08e4,在设计的小型蓝宝石腔中为50平方。此外,与我们的设计相比,法国的印度内部和IRCOM中的两个蓝宝石装载洞穴中的两个蓝宝石装载洞穴。

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