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Table 3

Results of fitting the parameters for AG Peg, for three assumed values of the inclination i, in the range 3090 degrees.

i = 30°
M 2 M 1 a M bol R L R 2 f = R2/RL vsini ϖ (mas)

0.8 0.5944 1.91 1.499 166.6 47.51 0.2851 1.481 2.299
1.0 0.6704 2.029 1.912 180.9 57.45 0.3176 1.791 1.901
1.3 0.7746 2.181 2.375 199.2 71.11 0.3569 2.217 1.536
1.6 0.8702 2.311 2.728 215.1 83.64 0.3889 2.607 1.306
2.0 0.9879 2.462 3.094 233.6 99.01 0.4238 3.087 1.103
2.5 1.123 2.626 3.449 253.8 116.6 0.4596 3.635 0.9366
3.0 1.249 2.769 3.733 271.5 132.9 0.4895 4.143 0.8219
3.5 1.368 2.897 3.969 287.6 148.2 0.5152 4.618 0.7373
4.0 1.48 3.014 4.171 302.2 162.6 0.538 5.068 0.6719

i = 50°
M 2 M 1 a M bol R L R 2 f = R2/RL vsini ϖ (mas)

0.8 0.339 1.785 1.499 174.5 47.51 0.2723 2.269 2.299
1.0 0.3865 1.906 1.912 189.6 57.45 0.303 2.744 1.901
1.3 0.4517 2.061 2.375 209.1 71.11 0.3402 3.396 1.536
1.6 0.5116 2.193 2.728 225.9 83.64 0.3703 3.995 1.306
2.0 0.5855 2.347 3.094 245.5 99.01 0.4032 4.729 1.103
2.5 0.6709 2.512 3.449 266.9 116.6 0.4369 5.57 0.9366
3.0 0.7503 2.656 3.733 285.8 132.9 0.4651 6.348 0.8219
3.5 0.8251 2.786 3.969 302.7 148.2 0.4894 7.076 0.7373
4.0 0.8963 2.903 4.171 318.3 162.6 0.5108 7.765 0.6719

i = 90°
M 2 M 1 a M bol R L R 2 f = R2/RL vsini ϖ (mas)

0.8 0.2452 1.735 1.499 180.1 47.51 0.2638 2.962 2.299
1.0 0.2808 1.857 1.912 195.7 57.45 0.2935 3.581 1.901
1.3 0.3298 2.012 2.375 215.9 71.11 0.3294 4.434 1.536
1.6 0.3748 2.145 2.728 233.4 83.64 0.3584 5.215 1.306
2.0 0.4304 2.299 3.094 253.7 99.01 0.3902 6.173 1.103
2.5 0.4947 2.464 3.449 275.9 116.6 0.4227 7.271 0.9366
3.0 0.5546 2.609 3.733 295.4 132.9 0.4499 8.286 0.8219
3.5 0.6111 2.739 3.969 313 148.2 0.4733 9.237 0.7373
4.0 0.6648 2.857 4.171 329.1 162.6 0.494 10.14 0.6719

Notes. In each case, we indicate the mass of the giant, M2; of its hot companion, M1; the semi-major axis, a (in AU); the bolometric magnitude; the Roche lobe radius, RL (in R); the radius of the giant, R2 (in R); the filling factor, f = R2/RL; the rotational velocity, vsini (in km s-1), assuming rotation is coplanar to the orbital motion; and the resulting parallax, ϖ, in mas.

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