Lunar Reconnaissance Orbiter Mission and Spacecraft Design

被引:1
|
作者
Craig R. Tooley
Martin B. Houghton
Richard S. Saylor
Cathy Peddie
David F. Everett
Charles L. Baker
Kristina N. Safdie
机构
[1] NASA’s Goddard Space Flight Center,
[2] Honeywell Technology Solutions Inc.,undefined
[3] Alliant Techsystems Inc.,undefined
来源
Space Science Reviews | 2010年 / 150卷
关键词
Lunar; Spacecraft; Mission design;
D O I
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中图分类号
学科分类号
摘要
Launched June 18, 2009, with its primary mission scheduled to end September 2010, NASA’s Lunar Reconnaissance Orbiter will be the first observatory ever to spend an entire year orbiting and observing the Moon at a low altitude of just 50 km. The spacecraft carries a wide variety of scientific instruments and will provide an extraordinary opportunity to study the lunar landscape at resolutions and over time scales never achieved before. This paper is intended as a companion to the series of papers released simultaneously in this journal detailing LRO’s instruments and their planned measurements. The paper describes the design and key performance drivers of the LRO spacecraft and overall mission design. It presents a comprehensive description of the operation of the various systems that comprise the spacecraft and illustrates how these systems enable achievement of the mission requirements.
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页码:23 / 62
页数:39
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