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Table 1

Parameters specific to the CDA and geometric parameters for the Enceladus flybys considered in this paper.

Flyby Date Data type Relative speed [km s−1] Detectable range of grains radii(a) [µm] Altitude at C/A [km] N Lat, W Lon of C/A Enceladus mean anomaly
E7 2 Nov. 2009 HRD 7.7 M1: (1.7,∞) 99 -89°, 137° 283°
M2: (3.1,∞)
M3: (6.7,∞)
m1: (1.8,∞)
m′2: (3.1,∞)
E21 28 Oct. 2015 HRD 8.5 M1: (1.6,∞) 49 −84°, 70° 84°
M2: (2.8,∞)
M3: (6.2,∞)
m1: (1.6,∞)
m2: (2.9,∞)
E5 9 Oct. 2008 DA 17.7 salt-poor: (0.2, 1.7) 25 −28°, 101° 208°
salt-rich: (0.1, 1.1)
E17 27 Mar. 2012 DA 7.5 salt-poor: (0.8, 6.2) 74 −86°, 154° 209°
salt-rich: (0.5, 4.1)
E18 14 Apr. 2012 DA 7.5 salt-poor: (0.8, 6.2) 74 −88°, 280° 200°
salt-rich: (0.5, 4.1)

Notes. The first column denotes the flyby, and the second column shows the CDA subsystem that obtained the data analyzed in this paper. The third column gives the velocity of the spacecraft relative to Enceladus. The fourth column denotes for E7 and E21 the HRD counters for which a rate profile was obtained, along with the range of grain radius the counter was sensitive to. For the E5, E17, and E18 encounters, this column gives the respective sensitive size range for the CA subsystem for salt-rich and salt-poor grains. Columns five, six, and eight give geometric parameters of the encounter, and column seven specifies the date of the flyby. (a)The derivation of the detectable size ranges for salt-poor and salt-rich particles (E5, E17, E18) is given in Sect. 2.1. The derivation of the HRD size thresholds is given in Sect. 2.3.

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