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Table B.1.

Properties of nonrotating NSs and rotating MSPs for the TM1 family.

L P Mmax ΔM Req(max) ΔR ρc(max) Req(1.4) e1.4 I1.4 Req(2.0) e2.0
(MeV) (ms) (M) (%) (km) (%) (fm−3) (km) (1) (1045 g cm2) (km) (1)
40 1 2.2441 5.57 12.545 6.02 0.8294 14.096 0.4901
40 2 2.1542 1.35 12.001 1.42 0.8907 13.605 0.3184 1.6010 13.017 0.2372
40 3 2.1383 0.60 11.909 0.64 0.8990 13.351 0.2128 1.6544 12.841 0.1568
40 5 2.1301 0.21 11.876 0.36 0.8990 13.226 0.1278 1.6818 12.753 0.0937
40 static 2.1256 0 11.833 0 0.9094 13.157 0 12.704 0

60 1 2.2408 5.59 12.647 6.88 0.8199 14.269 0.4987
60 2 2.1492 1.35 12.081 1.67 0.8805 13.850 0.3270 1.6176 13.104 0.2401
60 3 2.1330 0.60 11.960 0.65 0.8990 13.569 0.2183 1.6738 12.918 0.1586
60 5 2.1248 0.21 11.926 0.36 0.8990 13.433 0.1310 1.7024 12.824 0.0947
60 static 2.1202 0 11.883 0 0.9094 13.358 0 12.772 0

80 1 2.2432 5.79 12.788 6.69 0.8105 14.269 0.4987
80 2 2.1500 1.39 12.166 1.50 0.8805 14.181 0.3381 1.6580 13.270 0.2452
80 3 2.1335 0.61 12.068 0.68 0.8907 13.864 0.2256 1.7169 13.068 0.1619
80 5 2.1252 0.22 12.006 0.17 0.8990 13.710 0.1354 1.7468 12.968 0.0966
80 static 2.1205 0 11.986 0 0.8990 13.626 0 12.912 0

All configurations are computed within the Kepler limit, including the maximum rotational mass Mmax, the corresponding equatorial radius Req(max) and central number density ρc(max). ΔMR) refers to the change in the maximum mass (equatorial radius) with respect to the nonrotating configuration. The equatorial radius and the eccentricity of 1.4 M, 2 M MSPs are also shown.

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