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Table 2.

CE summary for J2102–4145, assuming a residual H mass M H fit = 10 7 M Mathematical equation: $ M_{\mathrm{H}}^\mathrm{{fit}} = 10^{-7}\,M_\odot $ that reproduces the observed radius of the secondary WD.

MZAMS Mcore Rphot ai Pi af ΔEorb Ebind αCE Eextra(α)
[M] [M] [R] [R] [day] [R] [1047 erg] [1047 erg] [1047 erg]
1.0 0.315 28.0 60.1 37.0 0.854 2.494 1.44 0.577  {α = 1 :   − ; α = 0.5 :  0.192}
1.5 0.315 25.1 50.1 26.6 0.854 2.402 2.41 1.003  {α = 1 :  0.007;  α = 0.5 :  1.21}
1.8 0.315 22.1 42.7 20.6 0.854 2.315 3.494 1.510  {α = 1 :  1.18;  α = 0.5 :  2.34}

Notes. anow = 0.80190 R (common to all three cases). Pi is the orbital period at CE onset, derived from ai through Kepler’s third law using M1, WD = 0.375 M. Eextra(α) denotes the additional energy required to reach the target α while keeping M H fit = 10 7 M Mathematical equation: $ M_{\mathrm{H}}^{\mathrm{fit}} = 10^{-7}\,M_\odot $. The orbital-energy change is computed from ai to af, and the binding energy from mcut to the stellar surface.

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