Antenna-rectifier for power supply subsystem of low-small spacecraft

D. Gretskih, A. Gomozov, V. Shokalo, S. F. A. Al-Sammarraie
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Abstract

An alternative way to get more electrical energy for small low-orbit spacecraft (SC), based on wireless power transmission by microwave beam from the surface to improve the energy balance of the spacecraft and spacecraft control capabilities for emergency contingency system in its orientation is offered. The receiving subsystem of a wireless energy transfer — antenna-rectifier (rectenna) was designed. Rectenna has a two-layer structure and receive the electromagnetic wave with circular polarization. To realize this, the radiating antenna structure and rectifier are implemented as a system of orthogonal microstrip collinear conductors with the integrated Schottky open-frame diodes.
小型航天器供电分系统天线整流器
提出了一种小型低轨航天器获取更多电能的替代方法,即利用地面微波波束无线传输电能,以改善航天器的能量平衡和航天器应急系统在其定位中的控制能力。设计了无线能量传输天线整流天线的接收分系统。整流天线采用两层结构,以圆极化方式接收电磁波。为了实现这一点,辐射天线结构和整流器被实现为与集成肖特基开框二极管的正交微带共线导体系统。
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