1984
DOI: 10.1016/0019-1035(84)90175-1
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Cratering rate over the surface of a synchronous satellite

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Cited by 49 publications
(43 citation statements)
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“…Asymmetries of impacts onto planets or satellites have been widely studied for synchronous rotating bodies (e.g. see Horedt & Neukum 1984;Marchi et al 2004). For non-synchronous rotating bodies, like Mercury, the same considerations hold, but now the asymmetry is related to the morning-evening (am/pm) hemispheres instead of to leading-trailing ones.…”
Section: Orbital and Diurnal Asymmetriesmentioning
confidence: 90%
“…Asymmetries of impacts onto planets or satellites have been widely studied for synchronous rotating bodies (e.g. see Horedt & Neukum 1984;Marchi et al 2004). For non-synchronous rotating bodies, like Mercury, the same considerations hold, but now the asymmetry is related to the morning-evening (am/pm) hemispheres instead of to leading-trailing ones.…”
Section: Orbital and Diurnal Asymmetriesmentioning
confidence: 90%
“…Planetocentric debris can crater symmetrically (Horedt and Neukum, 1984), but there does not appear to be a plausible source for large planetocentric objects in the jovian system. A 30-km-diameter crater on Ganymede implies a 2-km-diameter comet striking at 21 km/s, or a 5-km chunk of planetocentric debris striking at 5 km/s.…”
Section: Apex-antapex Asymmetriesmentioning
confidence: 96%
“…Morota and Furumoto (2003) have used these high quality images to count young rayed craters and concluded that a factor of 1.5 enhancement exists in the current cratering record when comparing fitted crater densities precisely at the apex to those directly at the antapex. An excess of leading-hemisphere craters is expected on synchronously-rotating satellites in general; Horedt and Neukum (1984) give expressions for the expected asymmetry caused by the leading hemisphere of the satellite "sweeping up" more objects. Based on such expressions and using their previous crater counts, Morota et al (2005) concluded that the measured leading enhancement implies an average impactor encounter speed with the Earth-Moon system of 12-16 km/s, consistent (though on the low end) with previous estimates (Shoemaker 1983;Chyba et al 1994).…”
Section: Introductionmentioning
confidence: 99%