LISA system design highlights
LISA system design highlights
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DOI：
10.1088/0264-9381/26/9/094015
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发表时间：
2009-04
影响因子：
3.5
通讯作者：
M. Sallusti;P. Gath;D. Weise;M. Berger;H. Schulte
中科院分区：
文献类型：
--
作者：
M. Sallusti;P. Gath;D. Weise;M. Berger;H. Schulte
2005年1月开始的一项合同授予了Astrium GmbH和Astrium Ltd的一个财团，用于制定丽莎使命。合同的范围是为使命结构和使命组成部分（特别侧重于有效载荷）制定一个参考设计，以及一个推导需求的连续阶段，最后将进行一次使命设计审查。技术起点是2000年发表的《最后技术报告》中正式确定的前一次丽莎研究的成果。在设计阶段，确定并权衡了不同的架构概念，包括丽莎轨道、测量方案和光机架构。在使命设计审查期间（2008年7月），提出了综合的使命基线设计、飞行要素和有效载荷子系统及主要部件的规格。本文简要介绍了最新设计的丽莎系统的主要设计要点。
A contract, started in January 2005, was awarded to a consortium of Astrium GmbH and Astrium Ltd for the LISA Mission Formulation. The scope of the contract was the development of a reference design for the mission architecture and for the mission elements (with particular focus on the payload) and a successive phase of derivation of requirements, to be concluded with a mission design review. The technical starting point was the output of the previous LISA study formalized in the Final Technical Report, issued in the year 2000. During the design phase, different architecture concepts were identified and traded off, including the LISA orbits, the measurement scheme and the opto-mechanical architecture. During the Mission Design Review (July 2008) the consolidated mission baseline design, and the specifications of the flight elements and of the payload subsystem and major components were presented. This paper gives a brief overview of the major design points of the latest design of the LISA system.