Table 2
Line fluxes.
Line | ν rest | Component | S line a,b | V cent a | V FWHM a |
![]() |
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.
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.
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%.
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