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Inflatable impulse radiating antenna for lunar penetrating radar

机译:探月雷达用充气脉冲辐射天线

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In this paper, an inflatable impulse radiating antenna (inf-IRA) that can be used in lunar penetrating radar application is described. The inf-IRA is covered by thin films as a main material so that it can be inflated as the air is injected and be packaged small size as the air is deflated. The reflector of inf-IRA, whose diameter and focal length are 0.3 m and 0.15 m, respectively, is made of reflective Mylar film. The parabolic curve is formed by joining planar discs. The structure is supported by attaching internal stays. Two feed arms are printed on a thin Kapton substrate. The arms are designed with an asymptotic conical dipole profile for low input impedance. The reflection coefficients and gain patterns of fabricated inf-IRA are measured and compared to those of simulation and rigid-IRA.
机译:在本文中,描述了一种可用于月球穿透雷达应用的充气式脉冲辐射天线(inf-IRA)。 inf-IRA被薄膜作为主要材料覆盖,因此可以在注入空气时将其充气,并在放气时将其包装成小尺寸。 inf-IRA的反射器的直径和焦距分别为0.3 m和0.15 m,由反射性聚酯薄膜制成。抛物线通过连接平面圆盘形成。该结构通过附加内部撑条得到支撑。在薄的Kapton基板上打印两个进纸臂。臂的设计采用渐近圆锥形偶极子外形,以实现低输入阻抗。测量了制成的inf-IRA的反射系数和增益模式,并将其与仿真和刚性IRA的反射系数和增益模式进行比较。

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