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Power system design and in orbit performance of Algeria's first micro satellite Alsat-1

机译:阿尔及利亚第一颗微卫星Alsat-1的动力系统设计和在轨性能

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摘要

On the 28th November 2002, Algeria's first enhanced micro satellite was launched into a 686 km low earth orbit onboard a Cosmos 3M rocket from Plesetsk. The spacecraft was designed, manufactured and launched as a technology transfer programme between the National Centre of Space Techniques (CNTS) Algeria and Surrey Satellite Technology Limited (SSTL) United Kingdom in the timescale of 18 months. This paper will describe the design and in orbit performance of the mission power system, stressing the decisions taken in order to meet the mission requirements within the 18 months, concept to launch programme. Most of the design and construction techniques used in the production of the Alsat-1 power system were based on SSTL heritage over the years. It will be shown how off the shelf components either for the generation or storage of the onboard energy can be applied successfully to such missions.
机译:2002年11月28日,阿尔及利亚的第一颗增强型微型卫星被普列塞茨克(Plesetsk)的Cosmos 3M火箭发射到了686公里的近地轨道。该航天器的设计,制造和发射是阿尔及利亚国家航天技术中心(CNTS)与英国萨里卫星技术有限公司(SSTL)之间的技术转让计划,时限为18个月。本文将介绍任务动力系统的设计和在轨性能,重点介绍为满足18个月内任务要求而做出的决策,发射计划的概念。多年来,Alsat-1电力系统生产中使用的大多数设计和建造技术都是基于SSTL的传统。将显示如何将现成的用于生成或存储车载能量的组件成功地应用于此类任务。

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