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Miniaturized Onboard System Components

机译:小型化的车载系统组件

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The introduction of stacked multi-chip-module (MCM) in 3D-System-in-Package (3D-SIP) enables a new level of integration in satellite systems, where the complete chain, from individual IC dies to system interfaces are miniaturized. Angstrom Aerospace Corporation has developed this concept, starting on the component packaging level, aiming for a step-by-step introduction of new standardized and modular satellite systems featureing plug and play. Three modules have been developed to demonstrate the technology and its performance. A general interface module (Remote Terminal Unit, RTU), a compact solid state mass memory module (MM) and a magnet torquer control module (MACS). The high packing density is achieved by MCM-D technology, based on silicon and LTCC substrates. By using silicon as carrier material, many advantages are obtained including the reduction of thermal stresses between the silicon based die and the packaging surrounding it. The mass of a distributed satellite bus is estimated to be less then 100 grams. Reducing the mass of systems with one to two magnitudes can improve existing mission concepts, but also enable new types of missions, only viable with a low mass high performance spacecraft.
机译:在3D系统级封装(3D-SIP)中引入了堆叠式多芯片模块(MCM),从而使卫星系统的集成度达到了新的高度,从而使从单个IC裸片到系统接口的完整链得以最小化。埃斯特罗姆航空航天公司已经从组件包装的水平开始发展这一概念,旨在逐步引入具有即插即用功能的新型标准化和模块化卫星系统。已经开发了三个模块来演示该技术及其性能。通用接口模块(远程终端单元,RTU),紧凑型固态海量存储模块(MM)和电磁转矩控制模块(MACS)。通过基于硅和LTCC基板的MCM-D技术可实现高封装密度。通过使用硅作为载体材料,可以获得许多优点,包括减少了硅基管芯与其周围的封装之间的热应力。分布式卫星总线的质量估计小于100克。将系统的质量降低一到两个数量级可以改善现有的任务概念,但也可以实现新型任务,只有在低质量高性能航天器中才可行。

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