2020
DOI: 10.1109/maes.2019.2950746
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Lunar Flashlight: Illuminating the Lunar South Pole

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Cited by 21 publications
(11 citation statements)
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“…The reflectance measurement precision at each lidar wavelength depends on the ability to accurately measure the transmitted laser pulse energy and the return pulse energy from the lidar. From these measurements (and the range to the surface) the lidar equation is used to retrieve the surface reflectance (Cohen et al., 2020; Lucey et al., 2014; Sun, 2017). The contribution of signal from thermal emission and solar reflectance was assumed to be removed using the continuous signal that is present between laser pulses when no laser illumination is present.…”
Section: Methodsmentioning
confidence: 99%
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“…The reflectance measurement precision at each lidar wavelength depends on the ability to accurately measure the transmitted laser pulse energy and the return pulse energy from the lidar. From these measurements (and the range to the surface) the lidar equation is used to retrieve the surface reflectance (Cohen et al., 2020; Lucey et al., 2014; Sun, 2017). The contribution of signal from thermal emission and solar reflectance was assumed to be removed using the continuous signal that is present between laser pulses when no laser illumination is present.…”
Section: Methodsmentioning
confidence: 99%
“…Single‐wavelength lidars with lasers emitting at 1.06 μm have identified regions with anomalous albedos at the northern pole of Mercury corresponding to regions of buried and exposed ice (Deutsch et al., 2017) and provided evidence supporting polar surface ice within lunar PSRs (Fisher et al., 2017; Lucey et al., 2014; Zuber et al., 2012). Soon the Lunar Flashlight technology demonstration will carry a multiband reflectometer emitting at four wavelengths between 1 and 2 μm (Cohen et al., 2020) to measure ISRU‐relevant quantities of water ice in select regions.…”
Section: Introductionmentioning
confidence: 99%
“…The spacecraft design is conservative, avoiding risky structures such as long composite booms or deployables while drawing upon heritage from previous missions for thermal management (Section 5.9), propulsion (Section 5.7), and attitude control (Section 5.8). The Sphinx avionics system on board AXE (see Section 5.4) is planned to gain flight heritage on various CubeSat missions as well (Cohen et al 2020).…”
Section: Flight Systemmentioning
confidence: 99%
“…These four missions all carry laser altimeters designed primarily for time-of-flight measurements, though with several new laser and detector technologies aimed at reducing the size and weight and increasing ranging precision. A notable exception is the upcoming Lunar Flashlight mission (Vinckier et al, 2019;Cohen et al, 2020), which carries a new class of laser reflectometer to measure the lunar surface reflectance at four key infrared wavelengths to constrain the abundance of surface water ice in permanently shadowed regions near the lunar South Pole. This instrument is not designed to provide accurate range measurements, but the quasi-CW operation is not dissimilar to traditional lidar, and we include it in our discussion here.…”
Section: Upcoming Lidar Investigationsmentioning
confidence: 99%