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Table 2

Line fluxes.

Line ν rest Component S line a,b V cent a V FWHM a a,b τ app c
(GHz) (mJy) (km s-1) (km s-1) (mJy km s-1)

CO J = 2–1 230.53800 Total ... ... ... (341 ± 51) × 103 ...

OH 4660 4.66024 Total ... ... ... −209 ± 11 ...
Main −1.18 ± 0.34 −18 ± 12 117 ± 18 −146 ± 35 0.039
Low velocity −0.46 ± 0.35 −116 ± 30 116 ± 54 −57 ± 35 0.015
Wing −0.29 ± 0.38 −247 ± 14 50 ± 53 −15 ± 12 0.009
OH 4751 4.75066 Total ... ... ... −534 ± 17 ...
Main −2.67 ± 0.18 7 ± 2 142 ± 7 −404 ± 18 0.091
Low velocity −0.94 ± 0.10 −113 ± 4 96 ± 8 −96 ± 6 0.031
Wing −0.36 ± 0.25 −239 ± 9 26 ± 13 −10 ± 5 0.012
Red wing −0.39 ± 0.21 170 ± 11 66 ± 25 −27 ± 10 0.013
OH 4766 4.76556 Total ... ... ... −296 ± 13 ...
Main −1.26 ± 0.11 17 ± 5 166 ± 11 −222 ± 12 0.042
Low velocity −0.43 ± 0.17 −129 ± 18 158 ± 51 −72 ± 17 0.014
OH 6017 6.01675 Total <0.19d ... ... ... ...
OH 6031 6.03075 Total ... ... ... −247 ± 9 ...
Main −1.31 ± 0.11 180 ± 6 e 132 ± 10 −184 ± 15 0.045
Low velocity −0.76 ± 0.14 109 ± 7 e 94 ± 14 −76 ± 13 0.026
OH 6035 6.03509 Total ... ... ... −410 ± 14 ...
Main −2.27 ± 0.16 −17 ± 5 121 ± 7 −292 ± 11 0.079
Low velocity −0.84 ± 0.33 −111 ± 3 85 ± 23 −75 ± 21 0.028
Wing −0.54 ± 0.34 −241 ± 14 71 ± 35 −41 ± 16 0.018
OH 6049 6.04909 Total <0.13d ... ... ... ...

Notes.

(a)

Parameters for individual components are derived from Gaussian fits to the global spectra and total line fluxes are derived from direct integration of the line profile.

(b)

The uncertainties in the VLA fluxes include an estimated 3% calibration error added in quadrature to the noise error. The calibration error in the SMA data is estimated to be 15%.

(c)

Apparent optical depth τapp = −ln(1 + Sline/Scont). A covering factor of 100% is assumed and τapp is thus a lower limit to the true optical depth.

(d)

1σ upper limit.

(e)

Relative to the 6035 MHz line which is located ~ 215 km s-1 below the 6031 MHz line.

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