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Table 1

Overview of the results after 10 kyr for all dust simulations carried out in this paper.

n (cm−3) Si destr. (%) Si destr. (M) C destr. (%) C destr. (M) vshockend$v_{{\rm{shock}}}^{{\rm{end}}}$ (km s−1)
1 0 56.8 1.46 35.5 0.91 388±3
1 0.3 53.0 ± 1.8 1.37 ± 0.05 33.0 ± 1.1 0.85 ± 0.03 348 ±3
1 1 45.6 ±2.7 1.53 ± 0.09 29.0 ± 1.5 0.97 ± 0.05 247 ± 18
1 3 42.7 ±3.6 1.49 ± 0.13 27.3 ± 2.7 0.95 ± 0.09 251 ± 26
10 0 91.7 5.63 76.9 4.72 226 ± 1
10 0.3 90.8 ±0.1 5.62 ± 0.01 76.3 ±0.1 4.72 ± 0.01 210±6
10 1 78.3 ±0.5 5.25 ± 0.03 63.0 ± 1.6 4.23 ± 0.11 198 ±16
10 3 57.6 ± 2.1 4.43 ± 0.16 45.5 ±3.9 3.50 ± 0.3 226 ± 21
100 0 86.9 9.23 87.2 9.26 127±4
100 0.3 86.9 ± 0.1 9.13 ± 0.02 87.0 ± 0.1 9.14 ± 0.01 128 ±3
100 1 81.0 ± 0.6 9.41 ± 0.06 79.2 ± 0.6 9.20 ± 0.06 125 ±5
100 3 75.9 ±0.9 11.0 ± 0.14 73.0 ±1.5 10.58 ± 0.22 88 ±1

1 0 55.5 1.42 33.0 0.85 388±3
1 0.3 51.7 ± 1.8 1.34 ± 0.05 30.4 ± 1.1 0.79 ± 0.03 348 ±3
1 1 44.8 ±2.7 1.5 ± 0.09 27.1 ± 1.5 0.91 ± 0.05 247 ± 18
1 3 41.8 ± 3.7 1.46 ± 0.13 25.3 ±2.6 0.88 ± 0.09 251 ± 26
10 0 91.0 5.58 74.2 4.55 226±1
10 0.3 90.1 ±0.1 5.57 ± 0.01 73.7 ±0.1 4.56 ± 0.01 210±6
10 1 75.4 ± 0.9 5.05 ± 0.06 55.8 ±0.4 3.74 ± 0.03 198 ±16
10 3 50.2 ±2.2 3.86 ± 0.17 33.1 ±1.2 2.55 ± 0.09 226 ± 21
100 0 69.8 7.41 63.1 6.7 127±4
100 0.3 70.6 ±0.5 7.43 ± 0.06 64.2 ± 0.6 6.75 ± 0.06 128 ±3
100 1 65.2 ± 3.1 7.57 ± 0.36 55.9 ± 3.2 6.49 ± 0.37 125 ±5
100 3 49.6 ±0.8 7.18 ± 0.11 36.6 ± 0.7 5.30 ± 0.10 88 ±1

Notes. The simulations vary in their considered average ISM density n, turbulent Mach number ℳ, and dust species. The values in the top 12 lines belong to the simulations that consider grain–grain collisions and sputtering, whereas the bottomM12 lines belong to the sputtering-only simulations. The values are averaged over three orthogonal 2D planes. Their standard deviation from the mean was used as the error of the mean. The average end shock velocity vshockend$v_{{\rm{shock}}}^{{\rm{end}}}$ was estimated by locating the SNR forward shock from a momentum threshold. The uncertainty in this value is due to the use of different thresholds, all of which trace the shock reasonably well.

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