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Ku波段150W空间行波管的设计和研制

Development of Ku-Band 150 W Space TWT

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【作者】 易红霞; 袁广江; 金锋; 王莉; 李延威; 陈之亮; 曹林林; 尚新文; 刘炎源; 戴志浩; 胡乃风; 李宁; 苏小保; 肖刘;

【Author】 YI Hong-xia;YUAN Guang-jiang;JIN Feng;WANG Li;LI Yan-wei;CHEN Zhi-liang;CAO Lin-lin;SHANG Xin-wen;LIU Yan-yuan;DAI Zhi-hao;HU Nai-feng;LI Ning;SU Xiao-bao;XIAO Liu;The Institute of Electronics,Chinese Academy of Sciences;

【机构】 中国科学院电子学研究所;

【摘要】 本文介绍了中科院电子所Ku波段150 W连续波空间行波管的设计、模拟和测试结果。该行波管采用双阳极电子枪、螺旋线跳渐变慢波结构、非轴对称四级降压收集极、辐冷型散热器。动态通过率在98.5%以上,在12.25~12.75 GHz范围内输出功率大于154 W,效率大于62%,增益大于51.8 dB,饱和点非线性相移小于46.65°,AM/PM变换系数小于4.31°/dB。环境试验结果表明行波管结构设计符合卫星力学环境条件,热设计符合空间环境试验条件。

【Abstract】 This paper reports the design,simulation work and test results of a Ku-band 150 W continuous wave space Traveling Wave Tube(TWT),which is fulfilled at the Institute of Electronics,ChineseAcademy of Sciences.The double-anode gun,helix pitch-tapering slow wave structure,non-axisymmetric four-stage depressed collector and radiation-cooled radiator are used in this TWT. The test results indicate that in the case of saturated drive,the TWT can get a power of over 154 W,an efficiency of over 62%,a gain of over 51. 8 dB,a phase shift less than46. 65°,and AM /PM factor less than 4. 31 deg /dB with the beam transmission rate of over 98. 5% in the operation band of 12. 25 ~ 12. 75 GHz. The environment testing was performed and the results show that the configuration design of this TWT is satisfiedfor a satellitemechanicsenvironment and the heat dissipation design is satisfied for an airborne environment.

【关键词】 空间行波管; Ku波段; 连续波; 辐冷型;
【Key words】 Space TWT; Ku-band; Continuous wave; Radiation-cooled;
  • 【文献出处】 真空电子技术 ,Vacuum Electronics , 编辑部邮箱 ,2014年03期
  • 【分类号】TN124
  • 【被引频次】2
  • 【下载频次】105
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