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Table 3.

Orbital evolution with different companions.

Model M2 [M] ai [R] tpi [d] npi api [R] Ppi [d] epi tf [d] nf af [R] Pf [d] ef
I.25 0.24 207 703 18.7 23 14 0.070 2000 151.5 17 10 0.032
I.50 0.49 236 766 13.9 41 29 0.033 2000 70.0 34 23 0.010
I.75 0.73 257 971 12.2 65 53 0.078 2000 38.5 55 41 0.083
O.25 0.24 207 1046 19.9 26 17 0.055 2500 124.2 22 13 0.008
O.50 0.49 236 840 9.2 50 39 0.059 2500 60.4 41 31 0.038
O.75 0.73 257 895 6.6 79 73 0.149 2500 32.6 69 57 0.102

Notes. The orbital separations a, the periods P, the times t, the numbers of orbits n and the eccentricities e are given for the end of the plunge-in with the subscript “pi” and for the end of the run with the subscript “f ”.

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