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. 2013 Dec 1;13(12):1155–1165. doi: 10.1089/ast.2013.1028

Table 5.

Probabilities and Estimated Viable Transfers over the Past 3.5 Gyr to Some of the Moons in the Outer Solar System

  Destination Impact ratio Probability (%) 3.5 Gyr total Mass transfer (kg)
from Earth
Io
7,300±900
5.7×10−6±7.0×10−7
10±1
3,800,000
 
Europa
15,000±2,000
2.8×10−6±5.0×10−7
6±0.9
1,900,000
 
Ganymede
13,000±2,000
3.1×10−6±5.0×10−7
6±1
2,100,000
 
Callisto
76,000±30,000
5.4×10−7±2.0×10−7
1±0.4
370,000
 
Enceladus
14,000±10,000
5.0×10−7±4.0×10−7
1±0.7
340,000
 
Titan
9,200±5,000
7.5×10−7±4.0×10−7
1±0.9
510,000
from Mars
Io
7,300±900
5.4×10−6±6.0×10−7
40±5
15,000,000
 
Europa
15,000±2,000
2.7×10−6±4.0×10−7
20±4
7,200,000
 
Ganymede
13,000±2,000
3.0×10−6±5.0×10−7
20±4
8,100,000
 
Callisto
76,000±30,000
5.2×10−7±2.0×10−7
4±2
1,400,000
 
Enceladus
14,000±10,000
<1.8×10−7
<1.4
<490,000
  Titan 9,200±5,000 <2.7×10−7 <2.1 <730,000

The impact ratio is the number of meteoroids that hit the planet (Jupiter or Saturn) for each one that hits the moon. For transfer from Mars to Saturn's moons, upper limits are used. The mass transfer rates are estimated by assuming that each transferred fragment is a sphere 3 m in diameter, with a density of 3 g/cm3, i.e., a mass of 340,000 kg each.