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Interdigital capacitor structure-based conformal traveling wave active antenna for experimental rocket communication

机译:基于代表电容器结构的保形行波主动天线,用于实验火箭通信

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This paper deals with the development of conformal traveling wave active antenna based on interdigital capacitor structure for 2.35MHz communication between an experimental rocket and the ground station. The proposed active antenna which has the dimension of 238.64mm × 45mm consists of 7 blocks of interdigital capacitor structure as antenna radiators connected with 6 pairs of RF amplifier as active components. All the components of active antenna are deployed on an RT/Duroid? 6010LM dielectric substrate with the thickness of 0.127mm. The use of very thin dielectric substrate for antenna realization is aimed to have a conformable antenna which fits the cylindrical body of experimental rocket. After obtaining the optimum performance design, the proposed active antenna is then realized through wet etching technique for experimental characterization. As comparison, a conformal traveling wave passive antenna is simultaneously developed and realized on the same dielectric substrate with the dimension of of 238.64mm × 22mm. From the characterization result, it shows that the realized active antenna resonates at center frequency of 2.3625GHz with gain of -16.648dBi. This result is slightly different with the realized passive antenna which resonates at center frequency of 2.375GHz with gain of -18.763dBi.
机译:这个保形行进的发展纸优惠基于针对实验火箭和地面站之间2.35MHz通信叉指电容器结构波有源天线。其具有238.64毫米×45毫米的尺寸所提出的有源天线包括叉指式电容器结构的7块作为具有6对RF放大器作为活性组分的连接天线辐射体。有源天线的所有组件被部署在一个RT /的Duroid? 6010LM电介质基板与0.127毫米的厚度。使用用于天线实现非常薄的电介质基板的旨在具有适合实验火箭的圆柱形主体的适形天线。获得最佳性能的设计之后,所提出的有源天线,然后通过对实验表征湿蚀刻技术来实现。作为比较,共形行波无源天线被同时开发并实现了与238.64毫米的×22毫米的尺寸相同的电介质基板上。从表征结果,它表明,在与-16.648dBi的增益2.3625GHz的中心频率的实现有源天线谐振。此结果与该谐振在与-18.763dBi的增益2.375GHz的中心频率的实现无源天线略有不同。

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