Lunar Reconnaissance Orbiter Mission 2010
DOI: 10.1007/978-1-4419-6391-8_12
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The Lunar Reconnaissance Orbiter Miniature Radio Frequency (Mini-RF) Technology Demonstration

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Cited by 26 publications
(31 citation statements)
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“…The Mini-RF flight instrument had to meet stringent mass and power constraints as well as accommodate a dual-linearly-polarized (H and V) antenna design as part of the technology demonstration theme of the experiment [Nozette et al, 2010;Raney et al, 2011]. Thus, an unusual analytical approach to look for ice was developed for the Mini-RF experiment [Raney, 2007].…”
Section: Experiments Design and Instrument Descriptionmentioning
confidence: 99%
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“…The Mini-RF flight instrument had to meet stringent mass and power constraints as well as accommodate a dual-linearly-polarized (H and V) antenna design as part of the technology demonstration theme of the experiment [Nozette et al, 2010;Raney et al, 2011]. Thus, an unusual analytical approach to look for ice was developed for the Mini-RF experiment [Raney, 2007].…”
Section: Experiments Design and Instrument Descriptionmentioning
confidence: 99%
“…The Lunar Reconnaissance Orbiter (LRO) mission payload was optimized to provide an abundance and diversity of data and information on the environment and deposits of the lunar polar regions [Chin et al, 2007]. The Mini-RF instrument is a synthetic aperture imaging radar that flew on both the Indian Space Research Organisation's Chandrayaan-1 (also called Mini-SAR (for miniature synthetic aperture radar) on that mission only) and on NASA's Lunar Reconnaissance Orbiter spacecraft [Spudis et al, 2009;Nozette et al, 2010;Raney et al, 2011]. Mini-RF was specifically designed to map the polar regions of the Moon, including the permanently dark, "cold-trap" areas, and characterize the RF properties and physical nature of the deposits there.…”
Section: Introductionmentioning
confidence: 99%
“…[12] Radar observations at 12.6 cm wavelength from both ground (Arecibo) and spacecraft (LRO Mini-RF [Nozette et al, 2010] total power images at higher spatial resolution) suggest a similar degree of roughness within and outside the sinuous melt feature making it indistinguishable from the surrounding melt deposit [B. Campbell and L. Carter, Pers. Comm.…”
Section: Surface Morphology and Texturementioning
confidence: 99%
“…Mini-RF on LRO (Nozette et al 2010;Raney et al 2011) is substantially more capable than the Chandrayaan-1 Forerunner, adding a second wavelength (X band, 4.2 cm), a 7.5 m/pixel zoom mode, and capabilities for interferometry and bistatic observations. Between the beginning of operations in 2009 July and the failure of the transmitter in 2010 December, the instrument obtained near-complete S-band zoom coverage of both poles to about 70°, with both eastward and westward look and illumination directions, as well as ~70% coverage from 80°-90° N in X-baseline mode.…”
Section: Lromentioning
confidence: 99%