Title :
Development of a Ku-band 150W space TWT
Author :
Xiao Liu ; Yi Hong-xia ; Yuan Guang-jiang ; Wang Li ; Li Yan-wei ; Chen Zhi-liang ; Cao Lin-lin ; Shang Xin-wen ; Su Xiao-bao
Author_Institution :
Inst. of Electron., Beijing, China
Abstract :
This paper reports the design, simulation work and test results of a 150W Ku-band continuous wave space Traveling Wave Tube (TWT), which is fulfilled at the Institute of Electronics, Chinese Academy 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 more than 154W, an efficiency of more than 62%, a phase shift less than 46.6 degree, and AM/PM factor less than 4.3deg/dB with the beam transmission rate of more than 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 satisfied for a satellite mechanics environment and the heat dissipation design is satisfied for an airborne environment.
Keywords :
anodes; cooling; electron guns; microwave tubes; satellite communication; slow wave structures; AM-PM factor; Chinese Academy of Sciences; Institute of Electronics; Ku-band continuous wave space traveling wave tube; Ku-band space TWT; airborne environment; beam transmission rate; double-anode gun; frequency 12.25 GHz to 12.75 GHz; heat dissipation design; helix pitch-tapering slow wave structure; nonaxisymmetric four-stage depressed collector; phase shift; power 150 W; radiation-cooled radiator; satellite mechanics environment; Aerospace electronics; Electron tubes; Gain; Power generation; Satellites; Space exploration; Temperature; Ku-band; Space TWT; continuous wave; radiation-cooled;
Conference_Titel :
Vacuum Electronics Conference (IVEC), 2015 IEEE International
Conference_Location :
Beijing
Print_ISBN :
978-1-4799-7109-1
DOI :
10.1109/IVEC.2015.7223917