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一种应用于星载InSAR系统的相位同步收发组件的设计

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为了提高星载InSAR系统星间同步信号的相位精度以提升卫星的测高精度,同时提高卫星在轨工作时间以提升卫星的成像能力,作为双星同步天线核心部件的相位同步收发组件,系统对其高功率发射、低噪声接收以及高效率的要求越来越高.基于MCM-C技术,采用机电热一体化设计,提出了一种兼具高功率发射、低噪声接收、高相位同步精度的高效率相位同步收发组件的设计方法.测试结果表明,组件接收状态下,接收增益在36 dB左右,噪声系数优于2.2 dB;发射状态下,饱和输出功率高于35 W,效率在37%左右.
Design of a phase synchronization T/R module for spaceborne InSAR systems
In order to enhance the phase precision of the spaceborne InSAR system's inter-satellite synchroni-zation signal so as to improve the satellite measure accuracy and simultaneously increase the satellite's in-orbit working time,so as to improve the satellite's imaging capability,the system has increasingly higher requirements for high-power transmission,low-noise reception and high efficiency of the phase synchronous T/R module,which is taken as the core component of the dual-satellite synchronous antenna.Based on MCM-C technology,this paper adopts electromechanical thermal integration design to propose a design method of high-efficiency phase synchronous transceiver module with high-power transmission,low-noise reception and high phase synchro-nization accuracy.The test results show that in the receiving state,the module receiving gain is about 36 dB,with the noise coefficient better than 2.2 dB;and that in the transmitting state,the saturated output power is higher than 35 W,with the efficiency about 37%.

spaceborne interferometric synthetic aperture radar(InSAR)MCM-C technologyphase continuity

傅熙、樊校生、秦超、王奇、吴小玲

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南京电子技术研究所,南京 210039

94916部队,南京 211599

星载干涉合成孔径雷达 MCM-C技术 相位连续性

2024

空天预警研究学报
空军预警学院

空天预警研究学报

影响因子:0.39
ISSN:2097-180X
年,卷(期):2024.38(6)