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首页> 外文期刊>Journal of Micromechanics and Microengineering >A modular assembly method of a feed and thruster system for Cubesats
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A modular assembly method of a feed and thruster system for Cubesats

机译:立方体卫星进给和推进器系统的模块化组装方法

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摘要

A modular assembly method for devices based on micro system technology is presented. The assembly method forms the foundation for a miniaturized feed and thruster system as part of a micro propulsion unit working as a simple blow-down system of a rocket engine. The micro rocket is designed to be used for constellation maintenance of Cubesats, which measure 10 × 10 × 10 cm and have a mass less than 1 kg. The feed and thruster system contains an active valve, control electronics, a particle filter and an axisymmetric converging-diverging nozzle, all fabricated as separate modules. A novel method is used to integrate these modules by placing them on or in a glass tube package. The assembly method is shown to be a valid method but the valve module needs to be improved considerably.
机译:提出了一种基于微系统技术的设备模块化组装方法。组装方法构成了微型进给和推进器系统的基础,该系统是微型推进单元的一部分,可作为火箭发动机的简单排污系统使用。该微型火箭旨在用于维护Cubesats的星座,其尺寸为10×10×10 cm,质量小于1 kg。进料和推进器系统包含一个主动阀,控制电子设备,一个粒子过滤器和一个轴对称的收敛-发散喷嘴,所有这些均制造为单独的模块。通过将这些模块放在玻璃管包装上或玻璃管包装中,可以使用一种新颖的方法来集成这些模块。组装方法被证明是有效的方法,但是阀模块需要大大改进。

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