Abstract
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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References
S. Andrews, M. Houghton, R. Saylor, Building fault tolerance into NASA’s Lunar Reconnaissance Orbiter. AAS 08-036, 2008
C. Baker et al., Lunar Reconnaissance Orbiter (LRO) rapid thermal design development, in International “Heat Pipe for Space Application” Conference, 2009
M. Beckman, Mission design for the Lunar Reconnaissance Orbiter, in AAS Guidance & Control Conference, 2007
G. Chin et al., Lunar Reconnaissance Orbiter: The instrument suite and mission. Space Sci. Rev. 129 (2007)
Department of Defense Interface Standard for Digital Time Division Command/Response Multiplex Data Bus, MIL-STD-1553B, 21 September 1978
ESA Standard, SpaceWire—links, nodes, routers and networks. ECSS-E-50-12C, 31 July 2008
D. Folta, D. Quinn, Lunar frozen orbits, in AAS/AIAA Astrodynamics Specialist Conference, 2006
L. Lee, Utilizing reliability predictions in space flight electronics designs, in International Military & Aerospace/Avionics COTS Conference, 2007
NASA Announcement of Opportunity, Lunar Reconnaissance Orbiter Measurement Investigations, NNH042SS00O, 18 June 2004
Q. Nguyen et al., A high performance command and data handling system for NASA’s Lunar Reconnaissance Orbiter. AIAA-2008-7926, 9 Sept. 2008
J. Wilmot, Implications of responsive space on the flight software architecture, in AIAA-RS4 2006-6003; AIAA Responsive Space Conference, 2006
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Tooley, C.R., Houghton, M.B., Saylor, R.S. et al. Lunar Reconnaissance Orbiter Mission and Spacecraft Design. Space Sci Rev 150, 23–62 (2010). https://doi.org/10.1007/s11214-009-9624-4
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DOI: https://doi.org/10.1007/s11214-009-9624-4