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Development of a High-Performance Low-Cost PPU for an Electrospray Colloid Electric Propulsion System for Small Satellite applications

机译:用于小型卫星应用的电喷雾胶体电动推进系统的高性能低成本PPU的开发

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The current state-of-art Electric Propulsion (EP) systems can provide impressive system performance but are associated with both significant volume requirements and high direct cost. These technologies have not been shown to be capable of being effectively scaled down in size, whilst retaining system performance. As a result, such technologies are not an established solution for nano- and micro satellites, which represent a rapidly increasing share of the market due to the advent of large constellations. Recognizing that the overall cost of an EP system is largely driven by the cost of the Power Processing Unit (PPU), a tailored low power, low cost and high performance PPU was designed targeting the CubeSat Market. By studying the periphery and interfaces, a straight-forward architecture was devised, containing 4 high voltage generators and 12 high voltage switches, all controlled by a microcontroller. The architecture is suited to drive two colloid thruster heads at opposite polarity, omitting the need of a neutralizer to keep the charge balance. The PPU is powered from a 5 V and 12V power bus and communicates via I~2C. The PPU is designed using low cost COTS (Commercial Of The Shelf) components, which were selected for high efficiency and high accuracy. To achieve high voltage accuracy, 4 calibrated, fine-tune regulation loops are implemented. The high voltage switch needed in this architecture requires a breakdown voltage of > 6 kV and needs to carry 3mA of current. Transistors for such a switch with breakdown voltages in the range of 6 kV are not available on the market. SystematIC is developing a high voltage stackable integrated circuit to provide a solution for the 6kV switch and enable implementation of the PPU architecture. During the bread board model testing we have verified that the maximum output power of a PPU with a volume of ? CubeSat cube is 20W. At full load the electrical efficiency of the overall PPU system is estimated to be about 80%. For an ou
机译:目前的最先进的电动推进(EP)系统可以提供令人印象深刻的系统性能,但与大量的体积要求和高直接成本相关。这些技术未被证明能够在尺寸的情况下有效地缩小,同时保持系统性能。结果,这种技术不是纳米和微卫星的建立解决方案,这代表了由于大星座的出现而迅速增加的市场份额。认识到,EP系统的总成本主要由电源处理单元(PPU)的成本而导致,定制低功耗,低成本和高性能PPU设计了立方体市场。通过研究外围和界面,设计了直接架构,其中包含4个高压发生器和12个高压开关,所有由微控制器控制。该架构很适合以相反的极性驱动两个胶体推进器头,省略中和剂的需要以保持电荷平衡。 PPU由5 V和12V电源总线供电,并通过I〜2C通信。 PPU采用低成本的婴儿床(商业架子)组件设计,这些元件被选择为高效率和高精度。为实现高压精度,实现了4个校准,精细调节循环。该架构中所需的高压开关需要> 6 kV的击穿电压,并且需要携带电流的3mA。用于这种开关的晶体管,在市场上没有击穿电压范围内的击穿电压。系统正在开发高压堆叠集成电路,为6kV开关提供解决方案,并实现PPU架构的实现。在面包板模型测试期间,我们已经验证了具有量的PPU的最大输出功率?立方体是20W。满载时,总PPU系统的电效率估计为约80%。对于OU.

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