Table A5.

Same as Table A3 but for HD 45995.

HJD-2 450 000.M1Mirror2-GaussianCorrelation
8446.91712.715.515.60.0
8462.81916.719.219.14.8
8520.68322.025.424.69.6
8546.62813.616.516.70.2
8886.72018.622.321.04.4
8898.65925.230.830.412.8
8946.59316.320.420.92.1
8948.62813.718.418.3−0.7
9112.99024.330.530.211.9
9165.81614.016.617.41.1
9166.82314.717.118.01.8
9195.80120.823.923.79.1
9217.79125.530.729.913.5
9238.71324.728.627.612.3
9248.64918.521.020.75.6
9252.68118.921.621.15.1
9301.60623.125.526.110.8
9312.57426.831.031.114.5
9494.99319.020.821.66.7
HJD-2 450 000.M1Mirror2-GaussianCorrelation
8446.91712.715.515.60.0
8462.81916.719.219.14.8
8520.68322.025.424.69.6
8546.62813.616.516.70.2
8886.72018.622.321.04.4
8898.65925.230.830.412.8
8946.59316.320.420.92.1
8948.62813.718.418.3−0.7
9112.99024.330.530.211.9
9165.81614.016.617.41.1
9166.82314.717.118.01.8
9195.80120.823.923.79.1
9217.79125.530.729.913.5
9238.71324.728.627.612.3
9248.64918.521.020.75.6
9252.68118.921.621.15.1
9301.60623.125.526.110.8
9312.57426.831.031.114.5
9494.99319.020.821.66.7

Note. The line was integrated from -−500 to 500 km s−1 for the moment method. Wings with normalized fluxes between 1.4 and 2.2 were used for the mirror method. The double Gaussians had center velocities ±a = ±220 km s−1.

Table A5.

Same as Table A3 but for HD 45995.

HJD-2 450 000.M1Mirror2-GaussianCorrelation
8446.91712.715.515.60.0
8462.81916.719.219.14.8
8520.68322.025.424.69.6
8546.62813.616.516.70.2
8886.72018.622.321.04.4
8898.65925.230.830.412.8
8946.59316.320.420.92.1
8948.62813.718.418.3−0.7
9112.99024.330.530.211.9
9165.81614.016.617.41.1
9166.82314.717.118.01.8
9195.80120.823.923.79.1
9217.79125.530.729.913.5
9238.71324.728.627.612.3
9248.64918.521.020.75.6
9252.68118.921.621.15.1
9301.60623.125.526.110.8
9312.57426.831.031.114.5
9494.99319.020.821.66.7
HJD-2 450 000.M1Mirror2-GaussianCorrelation
8446.91712.715.515.60.0
8462.81916.719.219.14.8
8520.68322.025.424.69.6
8546.62813.616.516.70.2
8886.72018.622.321.04.4
8898.65925.230.830.412.8
8946.59316.320.420.92.1
8948.62813.718.418.3−0.7
9112.99024.330.530.211.9
9165.81614.016.617.41.1
9166.82314.717.118.01.8
9195.80120.823.923.79.1
9217.79125.530.729.913.5
9238.71324.728.627.612.3
9248.64918.521.020.75.6
9252.68118.921.621.15.1
9301.60623.125.526.110.8
9312.57426.831.031.114.5
9494.99319.020.821.66.7

Note. The line was integrated from -−500 to 500 km s−1 for the moment method. Wings with normalized fluxes between 1.4 and 2.2 were used for the mirror method. The double Gaussians had center velocities ±a = ±220 km s−1.

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