Transition Region and Coronal Explorer Mission

I. J. Burt
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引用次数: 3

Abstract

The Transition Region and Coronal Explorer (TRACE) mission is the fourth mission in the Small Explorer (SMEX) program series at the National Aeronautics and Space Administration's Goddard Space Flight Center. The primary objective of the TRACE mission is to explore the connections between the fine scale magnetic fields in the solar surface and features in the solar photosphere, chromosphere, transition region, and corona. The TRACE spacecraft, including the instrument, weighs 250 kilograms, uses 200 watts of power, and will cost approximately 35 million dollars for the entire mission. It will launch into a Sun-synchronous Low Earth Orbit (LEO) in September 1997 and collect movie-like images of the Sun with one are second spatial and 1 second temporal resolution; these images will be made available on the Internet daily. This paper shows NASA's approach to small spacecraft development It discusses some trades in the design of each subsystem to accommodate instrument and spacecraft heritage as well as new mission requirements. Topics include: a solid state Command and Data Handling (C&DH) system, solid state memory using 20 Megabyte modules approximately 1"/spl times/1"/spl times/0.2" each; a fully digital Attitude Control System (ACS); a guide telescope fine error sensor for spacecraft attitude and control as well as image motion compensation to better than are second levels. Adaptations in ground systems and operations are also included as well as the systems engineering approach.
过渡区和日冕探测任务
过渡区和日冕探测器(TRACE)任务是美国国家航空航天局戈达德太空飞行中心小型探测器(SMEX)计划系列的第四个任务。TRACE任务的主要目标是探索太阳表面精细尺度磁场与太阳光球层、色球层、过渡区和日冕特征之间的联系。包括仪器在内的TRACE航天器重量为250公斤,功率为200瓦,整个任务将耗资约3500万美元。它将于1997年9月发射到太阳同步低地球轨道(LEO),以1秒的空间分辨率和1秒的时间分辨率收集太阳的电影图像;这些图片将每天在互联网上提供。本文展示了NASA的小型航天器开发方法,讨论了每个子系统设计中的一些交易,以适应仪器和航天器遗产以及新的任务要求。主题包括:固态命令和数据处理(C&DH)系统,使用20兆字节模块的固态存储器,每个模块约1"/spl次/1"/spl次/0.2";全数字姿态控制系统;一种制导望远镜精密误差传感器用于航天器姿态和控制以及像移补偿,以优于二级传感器。适应地面系统和操作也包括以及系统工程方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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