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3D-MCM MINIATURIZED SPACECRAFT PLATFORM MODULES

机译:3D-MCM微型太空船平台模块

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摘要

The introduction of micromachinery and small-scale processing enables a new level of integration in satellite systems, where the complete chain, from individual dies to system level is miniaturized. Angstrom Aerospace Corporation has been developing this concept, starting on the component packaging level, aiming for a step-by-step introduction of a whole new standardized and modular satellite system, the Microlink concept. Three modules are under development, a general interface module (CSIM), a compact mass memory module (MM) and a magnetotorquer control module (M-ACS). The high packing density is achieved by creating multi-chip-modules, based on silicon substrates, MCM-S. 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 the systems decrease remarkable, and further increase in functionality at this miniaturization level does not increase mass, only system complexity. The mass of the modules are estimated to be less then 100 grams, including a load-carrying frame structure. 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:微型机械和小规模加工的引入使卫星系统的集成度提高到一个新的水平,从单个模具到系统级的完整链被最小化。埃斯特罗姆航空航天公司一直在组件包装的层面上开发这种概念,旨在逐步引入全新的标准化和模块化卫星系统,即Microlink概念。三个模块正在开发中,一个是通用接口模块(CSIM),一个紧凑型大容量存储器模块(MM)和一个磁转矩控制模块(M-ACS)。通过基于硅基板MCM-S创建多芯片模块,可以实现高封装密度。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。系统的质量显着降低,并且在此微型化级别进一步提高功能不会增加质量,只会增加系统复杂性。包括承载框架结构在内,模块的质量估计不到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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