Table A18.

Same as Table A3 but for V810 Cas.

HJD-2 450 000.M1Mirror2-GaussianCorrelation
TIGRE
9418.885−31.8−36.8−36.10.0
9446.758−20.6−23.2−23.415.0
9496.744−29.9−35.2−34.43.8
CARMENES
8696.635−18.3−20.9−21.20.0
8712.641−21.4−24.8−24.7−2.4
8733.664−29.5−34.1−33.6−13.4
8756.478−21.7−27.5−27.6−2.2
8775.335−18.3−20.6−20.7−0.2
9416.652−30.6−35.8−35.4−15.0
9438.557−22.3−27.5−27.3−2.2
9457.632−18.8−21.0−21.5−0.3
9477.476−26.3−30.5−31.0−10.0
9502.448−25.6−31.8−31.8−7.3
HJD-2 450 000.M1Mirror2-GaussianCorrelation
TIGRE
9418.885−31.8−36.8−36.10.0
9446.758−20.6−23.2−23.415.0
9496.744−29.9−35.2−34.43.8
CARMENES
8696.635−18.3−20.9−21.20.0
8712.641−21.4−24.8−24.7−2.4
8733.664−29.5−34.1−33.6−13.4
8756.478−21.7−27.5−27.6−2.2
8775.335−18.3−20.6−20.7−0.2
9416.652−30.6−35.8−35.4−15.0
9438.557−22.3−27.5−27.3−2.2
9457.632−18.8−21.0−21.5−0.3
9477.476−26.3−30.5−31.0−10.0
9502.448−25.6−31.8−31.8−7.3

Note. The line was integrated from −500 to 500 km s−1 for the moment method. Wings with normalized fluxes between 1.6 and 2.8 were used for the mirror method. The double Gaussians had center velocities ±a = ±220 km s−1.

Table A18.

Same as Table A3 but for V810 Cas.

HJD-2 450 000.M1Mirror2-GaussianCorrelation
TIGRE
9418.885−31.8−36.8−36.10.0
9446.758−20.6−23.2−23.415.0
9496.744−29.9−35.2−34.43.8
CARMENES
8696.635−18.3−20.9−21.20.0
8712.641−21.4−24.8−24.7−2.4
8733.664−29.5−34.1−33.6−13.4
8756.478−21.7−27.5−27.6−2.2
8775.335−18.3−20.6−20.7−0.2
9416.652−30.6−35.8−35.4−15.0
9438.557−22.3−27.5−27.3−2.2
9457.632−18.8−21.0−21.5−0.3
9477.476−26.3−30.5−31.0−10.0
9502.448−25.6−31.8−31.8−7.3
HJD-2 450 000.M1Mirror2-GaussianCorrelation
TIGRE
9418.885−31.8−36.8−36.10.0
9446.758−20.6−23.2−23.415.0
9496.744−29.9−35.2−34.43.8
CARMENES
8696.635−18.3−20.9−21.20.0
8712.641−21.4−24.8−24.7−2.4
8733.664−29.5−34.1−33.6−13.4
8756.478−21.7−27.5−27.6−2.2
8775.335−18.3−20.6−20.7−0.2
9416.652−30.6−35.8−35.4−15.0
9438.557−22.3−27.5−27.3−2.2
9457.632−18.8−21.0−21.5−0.3
9477.476−26.3−30.5−31.0−10.0
9502.448−25.6−31.8−31.8−7.3

Note. The line was integrated from −500 to 500 km s−1 for the moment method. Wings with normalized fluxes between 1.6 and 2.8 were used for the mirror method. The double Gaussians had center velocities ±a = ±220 km s−1.

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