Ku波段150W空间行波管的设计和研制  

Development of Ku-Band 150 W Space TWT

作　　者：易红霞[1] 袁广江[1] 金锋[1] 王莉[1] 李延威[1] 陈之亮[1] 曹林林[1] 尚新文[1] 刘炎源[1] 戴志浩[1] 胡乃风 李宁[1] 苏小保[1] 肖刘[1] 

机构地区：[1]中国科学院电子学研究所,北京100190

出　　处：《真空电子技术》2014年第3期24-28,43,共6页Vacuum Electronics

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。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 

分 类 号：TN124[电子电信—物理电子学]