2016
DOI: 10.1016/j.icarus.2015.12.010
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Photometric characterization of the Chang’e-3 landing site using LROC NAC images

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Cited by 32 publications
(39 citation statements)
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“…Images from the LROC NAC taken after the landing revealed an area of increased reflectance interpreted as modification caused by rocket exhaust (Figure b) [ Clegg‐Watkins et al ., ]. Clegg‐Watkins et al [] performed a study of the CE‐3 landing site using LROC NAC images and found an increase in reflectance of ~10% within the blast zone relative to the background, similar to that at Apollo, Luna, and Surveyor landing sites. They reported changes in photometric behavior at the CE‐3 site consistent with decreased backscattering and smoothing of the surface.…”
Section: Datamentioning
confidence: 93%
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“…Images from the LROC NAC taken after the landing revealed an area of increased reflectance interpreted as modification caused by rocket exhaust (Figure b) [ Clegg‐Watkins et al ., ]. Clegg‐Watkins et al [] performed a study of the CE‐3 landing site using LROC NAC images and found an increase in reflectance of ~10% within the blast zone relative to the background, similar to that at Apollo, Luna, and Surveyor landing sites. They reported changes in photometric behavior at the CE‐3 site consistent with decreased backscattering and smoothing of the surface.…”
Section: Datamentioning
confidence: 93%
“…The locations of the four VNIS measurements (5 to 8) are shown. White dashed line outlines the blast zone; black dotted line highlights the rover tracks [ Clegg‐Watkins et al, ].…”
Section: Introductionmentioning
confidence: 99%
“…For more on the detailed physics and effects of plume effects during descent, we refer the reader to Lane et al (), Metzger et al (, ), Immer et al (), Immer et al (), Lane and Metzger (), Kaydash et al (), Clegg et al (), and Clegg‐Watkins et al ().…”
Section: Enhancing Technologiesmentioning
confidence: 99%
“…Using Lunar Reconnaissance Orbiter Camera narrow angle camera (LROC NAC) images to measure the extent of each blast zone, Clegg‐Watkins et al () found a consistent correlation between blast zone area and lander dry mass (Figure ), despite variations in descent trajectories, maneuvering, engine configuration, and spacecraft design. This relationship will serve as an important tool in predicting the scale of rocket exhaust effects for future landed missions.…”
Section: Enhancing Technologiesmentioning
confidence: 99%
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