STELLAR ASTROPHYSICS WITH A DISPERSED FOURIER TRANSFORM SPECTROGRAPH. II. ORBITS OF DOUBLE-LINED SPECTROSCOPIC BINARIES

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Published 2011 May 26 © 2011. The American Astronomical Society. All rights reserved.
, , Citation Bradford B. Behr et al 2011 AJ 142 6 DOI 10.1088/0004-6256/142/1/6

1538-3881/142/1/6

ABSTRACT

We present orbital parameters for six double-lined spectroscopic binaries (ι Pegasi, ω Draconis, 12 Boötis, V1143 Cygni, β Aurigae, and Mizar A) and two double-lined triple star systems (κ Pegasi and η Virginis). The orbital fits are based upon high-precision radial velocity (RV) observations made with a dispersed Fourier Transform Spectrograph, or dFTS, a new instrument that combines interferometric and dispersive elements. For some of the double-lined binaries with known inclination angles, the quality of our RV data permits us to determine the masses M1 and M2 of the stellar components with relative errors as small as 0.2%.

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1. INTRODUCTION

For the past several years, our research group has been developing a new optical spectrograph concept called the dispersed Fourier Transform Spectrograph, or dFTS. The instrument design merges a traditional Fourier Transform Spectrometer with a dispersive grating spectrograph such that the interferometer output is divided into thousands of narrowband channels, all operating in parallel. This multiplex advantage boosts the effective throughput of the system by a large factor, making the dFTS competitive with echelle spectrographs for spectroscopic analysis of stars, particularly measurement of their radial velocities (RVs).

Hajian et al. (2007) describe our prototype device, dFTS1, and explain the underlying theory and hardware implementation in detail. Based upon our commissioning observations with dFTS1, we subsequently designed and built a second-generation version, dFTS2, which we deployed to the Steward Observatory 2.3 m Bok Telescope for a year-long observing campaign. In Behr et al. (2009), we discuss the dFTS2 hardware and present velocimetry measurements of RV standard stars and single-lined spectroscopic binary stars (SB1s).

In this paper, we describe the results from our dFTS2 observations of double-lined spectroscopic binaries (SB2s) and double-lined triple systems. SB2s provide one of the best means for measuring the masses of stars: given an accurate RV curve for each stellar component and the inclination angle i of the orbital plane to the observer's line of sight, we can derive the component masses using Kepler's third law. Traditional spectroscopic observations with an echelle spectrograph and a thorium–argon calibration source can achieve a velocity precision of ∼0.01–0.10 km s−1 on late-type narrow-lined stars (Ramm et al. 2004; Skuljan et al. 2004; Tomkin & Fekel 2006; Fekel et al. 2007; Ramm 2008). For greater precision, Konacki (2005, 2009) has developed a technique using an iodine absorption cell with which the RVs of a spectroscopic binary can be measured at the 0.005–0.010 km s−1 level. Our dFTS2 instrument, in contrast, achieves high RV precision and stability without a superposed reference spectrum. As described in Behr et al. (2009), we measure the RVs of non-binary stars and single-lined binaries to 0.01–0.03 km s−1 and anticipate even better performance once thermal stability issues in our instrument design have been addressed.

2. DATA ACQUISITION AND RV ANALYSIS PROCEDURE

The data reported in this paper were collected between 2007 October and 2008 June during bright-time observing runs at the 2.3 m Bok Telescope of the Steward Observatory on Kitt Peak. An observation of a given SB2 target consisted of 500 exposures spanning a range of interferometer delays corresponding to a spectral resolution of approximately 50,000. Each exposure lasted 1.0–4.0 s in duration, depending on the star's brightness and the atmospheric seeing and opacity. Each scan also required a total overhead time of approximately four minutes, independent of exposure time, for CCD readout and moving to the next delay position. Our targets, listed in Table 1, were chosen because of their relative brightness and short periods, so that we could acquire many observations per star during the limited duration of this initial observing campaign.

Table 1. Spectroscopic Binary Targets Observed with dFTS2

Star V Magnitude Spectral Type P vsin iA, B References
      (days) (km s−1)  
ι Peg 3.8    F5V 10.21 7.6, 7.2 Fekel & Tomkin (1983)
ω Dra 4.8    F5V 5.28 7.1, 6.6 Mayor & Mazeh (1987), Fekel et al. (2009)
12 Boo 4.8    F8IV 9.60 13.1, 10.4 Boden et al. (2005), Tomkin & Fekel (2006)
V1143 Cyg 5.9    F5V 7.64 23.6, 36.2 Andersen et al. (1987)
β Aur 1.9    A2IV 3.96 34.5, 35.0 Smith (1948), Pourbaix (2000)
Mizar A 2.3    A2V 20.54 32.6, 36.2 Fehrenbach & Prevot (1961), Pourbaix (2000)
κ Peg 4.2    F5IV 5.97 7.1, 47.9 Mayor & Mazeh (1987), Hajian et al. (2007)
η Vir 3.9    A2V 71.79 5.1, 4.5 Hartkopf et al. (1992), Hummel et al. (2003)

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To measure double-lined RVs from our interferogram data, we employed a variation of the standard two-dimensional cross-correlation technique (Mazeh & Zucker 1994). Instead of transforming our interferograms into spectra and then cross-correlating model templates against each observed spectrum, we converted the template spectra into template interferograms and then compared those model interferograms to the observed interferograms. Because interferograms add linearly, we can compute sequences of single-lined interferograms for the A and B components of a binary, spanning a range of RVs for each, and then add together A and B interferograms to create a two-dimensional grid of double-lined model interferograms. Calculating the χ2 difference between the models and the observed interferogram data, we construct a map of fit quality, where the minimum point indicates the best-fit solution for component velocities V1 and V2, and the projection of the χ2 = χ2min + 2.30 contour line onto the V1 and V2 axes provides 1σ error bars on each RV point. The shapes of the χ2 contours were elliptical with minor and major axes aligned to the V1 and V2 axes, indicating no significant covariance between the component velocity errors.

For optimal results, the template spectra must be well matched to the actual spectra of the two stellar components. We generated synthetic spectra using the SPECTRUM spectral synthesis package (Gray & Corbally 1994; see also http://www.phys.appstate.edu/spectrum/spectrum.html) and then varied the transition strength log gf of each line and the projected rotation velocity vsin i for each stellar component to minimize the χ2 difference between the model and the observed data. A final template spectrum for each component was calculated from a median-filtered average of transition strengths from the individual observations, and the final two-dimensional RV cross-correlation was then performed using these templates. We found that we could derive relatively precise and self-consistent vsin i values from our interferograms (as listed in Table 1); a future paper will explore the use of dFTS data to measure stellar rotation velocities and other line broadening mechanisms.

Because our template spectra are generated using atomic transition wavelengths from the National Institute of Standards and Technology catalog, the derived RVs can be considered "accurate" in the sense that they reflect the total Doppler shift between the rest wavelength of a line and the observed wavelength. We have not (yet) attempted to tie our velocity scale to any IAU velocity standards, nor do we make any correction for gravitational redshift effects. The only adjustment made to the RV data is conversion to a solar system barycenter reference frame, using the IRAF tool bcvcorr. These barycentric RV data are listed in Table 2. It should be noted that for the κ Peg RVs, "V1" refers to the Bb component and "V2" refers to the A component.

Table 2. RV Data Measured with dFTS2

Star HJD − 2, 400, 000 Phase V1 (km s−1) V1 Error (km s−1) V2 (km s−1) V2 Error (km s−1)
ι Peg 54,400.6388 0.109 33.302 0.017 −64.348 0.080
ι Peg 54,401.7122 0.214 6.584 0.019 −21.902 0.091
ι Peg 54,401.7269 0.215 6.235 0.017 −20.958 0.084
ι Peg 54,402.6529 0.306 −20.809 0.021 22.781 0.109
ι Peg 54,403.6604 0.404 −44.161 0.020 59.933 0.103
ι Peg 54,404.6147 0.498 −52.709 0.032 73.279 0.196
ι Peg 54,604.9660 0.115 31.993 0.017 −62.573 0.080
ι Peg 54,606.9635 0.311 −22.230 0.015 24.831 0.067
ι Peg 54,634.8758 0.044 42.325 0.015 −78.934 0.067
ι Peg 54,634.8959 0.046 42.119 0.016 −78.687 0.072
ι Peg 54,635.9132 0.145 25.341 0.017 −51.490 0.076
ι Peg 54,635.9342 0.147 24.823 0.016 −50.598 0.075
ι Peg 54,637.8866 0.339 −29.723 0.017 36.656 0.073
ι Peg 54,637.9068 0.341 −30.242 0.017 37.434 0.080
ι Peg 54,638.9426 0.442 −49.514 0.015 68.427 0.066
ι Peg 54,638.9628 0.444 −49.713 0.015 68.752 0.064
ω Dra 54,547.9814 0.160 −48.332 0.027 29.389 0.049
ω Dra 54,549.9958 0.542 19.025 0.026 −53.678 0.046
ω Dra 54,578.9388 0.024 −44.148 0.031 24.305 0.056
ω Dra 54,579.9848 0.222 −41.842 0.027 21.495 0.050
ω Dra 54,603.8020 0.733 13.203 0.024 −46.284 0.045
ω Dra 54,603.9267 0.756 9.247 0.029 −41.483 0.054
ω Dra 54,604.9389 0.948 −31.906 0.026 9.346 0.049
ω Dra 54,605.8126 0.114 −49.790 0.023 31.110 0.041
ω Dra 54,605.9378 0.137 −49.461 0.026 30.731 0.048
ω Dra 54,634.9202 0.627 22.606 0.025 −57.902 0.046
ω Dra 54,634.9758 0.637 22.298 0.023 −57.528 0.040
ω Dra 54,635.6924 0.773 6.250 0.022 −37.884 0.039
ω Dra 54,636.6824 0.960 −34.305 0.024 12.288 0.042
ω Dra 54,636.9410 0.009 −42.260 0.022 22.042 0.039
ω Dra 54,637.6927 0.152 −48.736 0.027 29.976 0.049
ω Dra 54,637.9312 0.197 −45.017 0.026 25.330 0.047
12 Boo 54,547.9153 0.591 −29.048 0.065 50.273 0.072
12 Boo 54,548.9127 0.694 −48.375 0.076 70.324 0.083
12 Boo 54,549.9111 0.798 −51.801 0.080 73.760 0.093
12 Boo 54,577.7996 0.702 −49.395 0.049 71.239 0.056
12 Boo 54,579.8185 0.912 −18.824 0.060 39.831 0.070
12 Boo 54,579.8722 0.918 −16.030 0.054 37.061 0.062
12 Boo 54,602.8623 0.312 50.008 0.070 −31.349 0.079
12 Boo 54,603.7304 0.402 22.867 0.073 −3.201 0.084
12 Boo 54,604.7012 0.503 −6.315 0.061 26.942 0.071
12 Boo 54,605.7012 0.607 −32.713 0.055 53.903 0.065
12 Boo 54,606.6579 0.707 −49.876 0.063 71.703 0.071
12 Boo 54,635.7226 0.733 −52.290 0.064 74.099 0.073
12 Boo 54,638.7263 0.046 58.158 0.084 −39.386 0.092
V1143 Cyg 54,603.8512 0.742 6.959 0.260 −39.988 0.490
V1143 Cyg 54,604.8585 0.873 57.691 0.200 −92.635 0.333
V1143 Cyg 54,605.8830 0.007 59.725 0.191 −95.517 0.309
V1143 Cyg 54,606.8736 0.137 −69.958 0.250 37.136 0.445
V1143 Cyg 54,634.8268 0.796 22.287 0.168 −55.975 0.320
V1143 Cyg 54,636.8467 0.060 −29.744 0.205 −0.671 0.339
V1143 Cyg 54,638.8573 0.323 −65.668 0.192 33.420 0.335
β Aur 54,400.9449 0.134 54.375 0.151 −91.605 0.149
β Aur 54,401.9169 0.379 −96.561 0.158 63.013 0.156
β Aur 54,402.9819 0.648 −81.719 0.193 48.833 0.195
β Aur 54,402.9909 0.651 −81.088 0.169 47.313 0.170
β Aur 54,403.8922 0.878 60.619 0.289 −98.087 0.286
β Aur 54,403.8982 0.880 61.415 0.203 −98.274 0.196
β Aur 54,404.8387 0.117 62.259 0.292 −99.681 0.290
β Aur 54,404.8542 0.121 60.690 0.241 −97.396 0.236
β Aur 54,404.8680 0.125 58.476 0.253 −95.754 0.244
β Aur 54,487.7015 0.042 86.798 0.292 −124.300 0.274
β Aur 54,487.7106 0.044 86.270 0.237 −124.136 0.236
β Aur 54,487.7191 0.046 86.305 0.381 −123.834 0.374
β Aur 54,487.7530 0.055 84.279 0.550 −122.404 0.556
β Aur 54,488.7643 0.310 −56.848 0.217 23.889 0.209
β Aur 54,488.7731 0.312 −58.307 0.206 24.076 0.203
β Aur 54,488.7818 0.315 −59.895 0.200 26.191 0.196
β Aur 54,491.6686 0.044 85.997 0.288 −124.270 0.283
β Aur 54,491.6835 0.047 85.742 0.159 −123.753 0.159
β Aur 54,491.7588 0.066 81.639 0.350 −119.413 0.341
β Aur 54,491.7881 0.074 79.167 0.413 −116.398 0.395
Mizar 54,488.9333 0.660 21.818 0.361 −37.796 0.408
Mizar 54,488.9434 0.661 22.811 0.980 −37.749 1.093
Mizar 54,488.9518 0.661 22.457 0.312 −37.301 0.394
Mizar 54,488.9604 0.662 23.821 0.556 −37.302 0.708
Mizar 54,492.0078 0.810 44.126 0.247 −57.208 0.329
Mizar 54,492.0468 0.812 43.908 0.354 −57.704 0.456
Mizar 54,548.8658 0.578 11.679 0.482 −26.290 0.640
Mizar 54,549.8253 0.625 17.287 0.174 −32.974 0.222
Mizar 54,576.7827 0.937 39.127 0.417 −52.615 0.543
Mizar 54,578.7569 0.034 −74.826 0.211 59.789 0.266
Mizar 54,579.7472 0.082 −81.159 0.264 66.865 0.333
Mizar 54,579.7558 0.082 −81.404 0.289 66.645 0.366
Mizar 54,602.7619 0.202 −52.427 0.283 37.381 0.368
Mizar 54,603.6351 0.245 −42.830 0.240 27.669 0.301
Mizar 54,604.6286 0.293 −33.460 0.289 19.960 0.377
Mizar 54,634.6759 0.756 36.381 0.306 −49.740 0.402
Mizar 54,636.6348 0.851 48.098 0.184 −61.666 0.246
Mizar 54,637.6408 0.900 48.821 0.213 −62.867 0.287
κ Peg 54,400.6227 0.069 26.262 0.031 2.603 0.361
κ Peg 54,401.6788 0.245 −10.951 0.035 −0.613 0.345
κ Peg 54,402.6158 0.402 −46.681 0.055 4.407 0.415
κ Peg 54,402.6305 0.405 −47.035 0.064 3.843 0.465
κ Peg 54,403.6430 0.574 −49.989 0.039 0.649 0.309
κ Peg 54,404.5841 0.732 −16.839 0.042 −0.683 0.416
κ Peg 54,404.5988 0.734 −16.173 0.054 0.520 0.506
κ Peg 54,634.8531 0.294 −24.846 0.029 0.465 0.317
κ Peg 54,635.8924 0.468 −55.088 0.032 −0.740 0.284
κ Peg 54,636.8741 0.632 −41.896 0.035 6.552 0.275
κ Peg 54,637.8349 0.793 −2.007 0.034 0.883 0.333
η Vir 54,491.9611 0.229 11.665 0.022 −11.833 0.067
η Vir 54,548.8113 0.021 −27.988 0.034 40.160 0.101
η Vir 54,549.7519 0.034 −26.057 0.030 37.392 0.090
η Vir 54,576.7011 0.409 21.091 0.035 −25.264 0.099
η Vir 54,577.7526 0.424 21.138 0.035 −25.293 0.105
η Vir 54,579.7025 0.451 20.923 0.039 −25.080 0.119
η Vir 54,603.7043 0.785 −6.225 0.028 10.650 0.085
η Vir 54,604.6471 0.799 −8.312 0.029 13.633 0.087
η Vir 54,605.6656 0.813 −10.717 0.030 16.643 0.091
η Vir 54,634.6939 0.217 9.759 0.033 −10.524 0.101
η Vir 54,636.6521 0.244 12.931 0.026 −14.812 0.076

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We derived orbital parameters from our RV data points using the IDL routines CURVEFIT, a gradient-expansion nonlinear least-squares fitting algorithm included with the IDL package, and HELIO_RV (Landsman 1993), which computes a line-of-sight velocity curve for a binary component given the period P, periastron time T (or for circular orbits, the time of maximum positive velocity), eccentricity e, periastron longitude ω, RV semi-amplitude K, and systemic velocity V0 (alternatively denoted as γ by some researchers). We fit the primary and secondary RV points simultaneously, assuming that P, T, e, and V0 are the same for both components and that ω1 and ω2 differ by 180°. The CURVEFIT routine returns 1σ uncertainties (standard deviations) for all derived parameters. For all of our SB2 targets, we adopted the orbital period P from previously published analyses because our observations covered a relatively short period of time. We did not correct for the light travel time across each binary system, because the resulting changes in the RV values are small compared to the RV error bars in all six cases.

3. RESULTS FOR DOUBLE-LINED BINARY SYSTEMS

3.1. ι Pegasi

Our RV measurements for the double-lined spectroscopic binary ι Pegasi (HR 8430, HD 210027, and HIP 109176) are plotted in Figure 1. The most recent published RV work on this system comes from Fekel & Tomkin (1983) whose orbital parameters are listed in Table 3 along with the values that we derive from our dFTS2 observations. In addition to adopting their value of the system's orbital period, we also followed their lead in assuming a circular orbit, because our RV points only covered half of the orbital phase, and CURVEFIT could not place meaningful constraints on e or ω. Our values for K1 and K2 are compatible with those of Fekel & Tomkin, although our solution for V0 differs by a statistically significant amount. This discrepancy may indicate the gravitational influence of an unseen and distant third stellar component of the system, although Tokovinin et al. (2006) did not find any close tertiary companions in Two Micron All Sky Survey images of ι Peg, and the astrometric observations of Boden et al. (1999) saw no evidence for a companion either. Alternatively, the difference in V0 might merely be a result of different RV zero points between Fekel & Tomkin's observations and ours—unfortunately, we did not make any RV observations of ι Piscium, the RV standard star that they used as their reference spectrum.

Figure 1.

Figure 1. RV measurements of the SB2 system ι Pegasi. Filled squares show the measured RV of the primary component, and open squares indicate the secondary component. Our observing campaign had ended before we were able to complete the phase coverage of this system.

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Table 3. Orbital Parameters and Stellar Mass Estimates for ι Pegasi

Parameter Fekel & Tomkin (1983) This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 10.213033 ± 0.000013 adopted from F&T adopted from F&T
T (reduced HJD) 45320.1423 54399.5296 ± 0.0003 54399.5288 ± 0.0007
e 0.0 assumed 0.0 assumed 0.0 assumed
K1 (km s−1) 48.1 ± 0.2 48.380 ± 0.006 48.380 ± 0.018
K2 (km s−1) 77.9 ± 0.3 77.637 ± 0.027 77.638 ± 0.050
V0 (km s−1) −5.5 ± 0.2 −4.245 ± 0.007 −4.229 ± 0.015
Nobs  32    16    16
χ2 primary  ...    142.20    16.45
χ2 secondary  ...    64.52    16.11
σRV primary (km s−1) 0.90    0.056    0.059
σRV secondary (km s−1) 1.16    0.158    0.156
M1 (M) 1.326 ± 0.016a 1.3239 ± 0.0018 1.3239 ± 0.0025
M2 (M) 0.819 ± 0.009a 0.8250 ± 0.0010 0.8250 ± 0.0013

Note. aFrom Boden et al. (1999), using F&T velocities in conjunction with spatial interferometer observations.

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Although the rms scatter of our RV points around the best-fit orbital curves is small (56 m s−1 and 158 m s−1 for the A and B components, respectively), the scatter is larger than would be expected from the error bars on each individual RV measurement, and is significantly above the instrumental RV error floor of ∼10 m s−1 that we determined in Behr et al. (2009). To account for this discrepancy, we multiply the RV error bars by 3.11 for the primary and 1.83 for the secondary, such that the mean per-measurement error bar matches the rms deviation σRV for each stellar component. The orbital fits are then recalculated using these scaled error bars, and the resulting orbital parameters are listed in the rightmost column of Table 3. This same procedure is applied to all subsequent binary systems as well.

The additional RV variability, if real, may be a result of stellar activity on both the primary and secondary, driven by tidal interactions between the two stars. Fekel & Tomkin measure vsin i = 7 ± 2 km s−1 for the primary, very close to an estimated synchronous rate of 6.5 km s−1, and vsin i = 9 ± 3 km s−1 for the secondary, which is well above the estimated synchronous rate of 4.5 km s−1. Gray (1984) finds vsin i values of 6.5 ± 0.3 km s−1 (primary) and 5 ± 1 km s−1 (secondary), suggesting that the system is synchronized. Our preliminary analysis of line broadening indicates vsin i = 7.6 and 7.2 for the primary and secondary, respectively. If the secondary is indeed spinning more rapidly than the synchronous rate, then above-average surface activity could result, which would add significant astrophysical RV "jitter" to our measurements. A synchronously rotating component would be less susceptible to tidal effects, but activity might still be enhanced by the proximity of a massive companion. However, Konacki et al. (2009) measured RVs of ι Peg with three different spectrographs and found no jitter greater than 17 m s−1 (primary) and 85 m s−1 (secondary), suggesting that the jitter observed by dFTS2 was instrumental rather than astrophysical.

Boden et al. (1999) measured an inclination angle for this system of i = 95fdg67 ± 0fdg22 (based on their primary data set). Using this value along with our orbital parameters, with the fundamental parameters recommended by Torres et al. (2010), we derive stellar masses of M1 = 1.3241 ± 0.0018 M and M2 = 0.8251 ± 0.0010 M, which represent relative (statistical) errors of 0.14% and 0.12%, respectively. With scaled error bars, the mass estimates are the same, albeit with larger error bars, for relative uncertainties of 0.19% and 0.15%. These values agree reasonably well with the calculations of Boden et al. who used Fekel & Tomkin's K1 and K2 values to determine M1 = 1.326 ± 0.016 M and M2 = 0.819 ± 0.009 M. For our mass estimates, the largest component of the error budget is due to the uncertainty in i, although the uncertainties in the K values are also significant contributors.

3.2. ω Draconis

The spectroscopic orbit of the ω Draconis system (HR 6596, HD 160922, and HIP 86201) was measured by Mayor & Mazeh (1987) and more recently by Fekel et al. (2009). Their derived orbital parameters are shown in Table 4, along with our values. Our K velocities agree closely with those of Fekel et al. We find a small but non-zero eccentricity for the orbits, 0.0023 ± 0.0002. Fekel et al. derived e = 0.0027 ± 0.0008 for the primary, with ω1 = 40fdg1 ± 17fdg8 (F. C. Fekel 2009, private communication), but their e and ω values for the secondary did not agree with those of the primary, so they adopted a circular orbit for the system. (Our ω1 = 137.86 ± 13.48, as described below.) Despite the similarity between our e value and their non-zero e value, the measurements of ω1 are substantially different, so we cannot plausibly claim that an orbital eccentricity has been clearly detected.

Table 4. Orbital Parameters and Stellar Mass Estimates for ω Draconis

Parameter Mayor & Mazeh (1987) Fekel et al. (2009) This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 5.279799 ± 0.000003 5.2798088 ± 0.0000083 adopted from Fekel et al. adopted from Fekel et al.
T (reduced HJD) 44698.273 ± 0.005 53980.1606 ± 0.0006 54547.1347 ± 0.0753 54547.1180 ± 0.1974
e 0 0.0 assumed    0.0023 ± 0.0002a 0.0023 ± 0.0006
ω1 (deg) ... ... 139.01 ± 5.14 137.86 ± 13.48
K1 (km s−1) 35.8 ± 0.3 36.326 ± 0.029 36.293 ± 0.008 36.292 ± 0.020
K2 (km s−1) 45.2 ± 0.3 44.699 ± 0.039 44.717 ± 0.014 44.718 ± 0.038
V0 (km s−1) −14.1 ± 0.2 −13.975 ± 0.018 −13.497 ± 0.006 −13.501 ± 0.016
Nobs 27 82    16    16
χ2 primary ... ...    92.10    15.42
χ2 secondary ... ...    138.65    19.42
σRV primary (km s−1) ... 0.19 (unit weight)    0.061    0.059
σRV secondary (km s−1) ... ...    0.126    0.126
M1sin 3i (M) 0.163 ± 0.003 0.16090 ± 0.00032 0.16054 ± 0.00011 0.16054 ± 0.00030
M2sin 3i (M) 0.129 ± 0.002 0.13076 ± 0.00024 0.13030 ± 0.00007 0.13029 ± 0.00018

Note. aBut see the text regarding the validity of this non-zero eccentricity.

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As an additional test of the non-zero eccentricity, we follow the Fekel et al. procedure of fitting orbits to the A and B components separately and comparing the derived values for ω1 and ω2, which should differ by 180°. Using the formal error bar data, we calculated e1 = 0.0020 ± 0.0003 with ω1 = 74fdg16 ± 12fdg74, and e2 = 0.0027 ± 0.0005 with ω2 = 243fdg14 ± 13fdg05. The eccentricity values agree reasonably well, and the ω angles differ by ∼169°, which is within 1σ of 180°. However, this ω1 value does not agree with the ω1 value from the combined fit, which is puzzling. This discrepancy may be related to the apparent systematic trends in the secondary RV residuals which are evident in Figure 2. Further observations with better phase coverage will be required to validate or refute our measured eccentricity for ω Dra.

Figure 2.

Figure 2. RV measurements of the SB2 system ω Draconis.

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As with ι Peg, our value for V0 differs from the prior work by a statistically significant amount, although the magnitude of the difference is not as large. Differences in the RV zero point are the most likely explanation.

No visual orbit or estimate of the inclination angle i has been determined for this binary, despite efforts to resolve it using speckle interferometry (Isobe 1991; Miura et al. 1995). We are therefore unable to calculate the true masses of the stellar components. We find M1sin 3i = 0.16054 ± 0.00011 M and M2sin 3i = 0.13030 ± 0.00007 M, in moderately good agreement with Fekel et al. (With the scaled RV error bars, our mass estimates are virtually unchanged, with error bars approximately three times larger.) We hope that long-baseline interferometers will soon be able to resolve the astrometric orbit of this system and determine the inclination angle.

3.3. 12 Boötis

The spectroscopic binary 12 Boötis (HR 5304, HD 123999, and HIP 69226) has received recent attention from both Boden et al. (2005), who combined spectroscopic and astrometric data, and Tomkin & Fekel (2006), who performed a high-precision spectroscopy-only assessment of the orbit. Orbital parameters are shown in Table 5, and our RV data are plotted in Figure 3. The derived quantities for e and ω1 are in excellent agreement among all three studies. Our K1 and K2 values, on the other hand, are smaller than those of Boden et al. and Tomkin & Fekel by several standard deviations, and our derived systemic velocity is different as well. The discrepancy in V0 may simply be ascribed to a different RV zero point, but the difference in K1/2 deserves further scrutiny. Due to the premature conclusion of our observing program, our RV data do not fully cover the region of maximum absolute velocities around phase =0.15, so the velocity amplitudes are not as reliably constrained as they might be. When dFTS observations resume, 12 Boo will be one of our highest priority targets, so that this issue can be addressed.

Figure 3.

Figure 3. RV measurements of the SB2 system 12 Boötis.

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Table 5. Orbital Parameters and Stellar Mass Estimates for 12 Boötis

Parameter Boden et al. (2005)a Tomkin & Fekel (2006) This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 9.6045492 ± 0.0000076 9.6045529 ± 0.0000048 adopted from T&F adopted from T&F
T (reduced HJD) 51237.7729 ± 0.0051 52400.4292 ± 0.0035 54542.2431 ± 0.0031 54542.2424 ± 0.0042
e 0.19233 ± 0.00086 0.19268 ± 0.00042 0.1928 ± 0.0003 0.1928 ± 0.0004
ω1 (deg) 286.67 ± 0.19 286.87 ± 0.14 286.79 ± 0.12 286.78 ± 0.17
K1 (km s−1) 67.302 ± 0.087 67.286 ± 0.037 67.107 ± 0.035 67.113 ± 0.047
K2 (km s−1) 69.36 ± 0.10 69.30 ± 0.05 69.110 ± 0.037 69.102 ± 0.054
V0 (km s−1) 9.551 ± 0.051 9.578 ± 0.022 10.040 ± 0.018 10.046 ± 0.025
Nobs 49 24    13    13
χ2 primary ∼49.0 ...    17.87    10.16
χ2 secondary ∼49.0 ...    30.79    14.02
σRV primary (km s−1) 0.47 0.11    0.082    0.077
σRV secondary (km s−1) 0.54 ...    0.115    0.119
M1 (M) 1.4160 ± 0.0049 1.416 ± 0.003 1.4013 ± 0.0025 1.4011 ± 0.0031
M2 (M) 1.3740 ± 0.0045 1.375 ± 0.002 1.3607 ± 0.0024 1.3608 ± 0.0028

Note. aCombined fit to RV and astrometric data.

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Given smaller K amplitudes than prior publications, we derive smaller masses as well. Using i = 107fdg990 ± 0fdg077 from Boden et al., we determine M1 = 1.4013 ± 0.0025 M and M2 = 1.3607 ± 0.0024 M, for a relative statistical uncertainty of 0.18%. These values are several σ smaller than the masses derived by Boden et al. and Tomkin & Fekel.

3.4. V1143 Cygni

The eclipsing SB2 system of V1143 Cygni (HR 7484, HD 185912, and HIP 96620) was previously analyzed by Andersen et al. (1987). Their orbital parameters are compared to ours in Table 6, and our RV data are plotted in Figure 4. There is a broad agreement between the two sets of orbital elements, although the error bars that we derived for K1 and K2 are relatively large, partly because of the small number of observations, partly because the individual RV measurements had larger error bars due to larger rotational broadening of the absorption lines and lower signal-to-noise ratio. Of particular interest is the comparison of the periastron angle ω1. From precise photometric timing of the system's eclipses, Gimenez & Margrave (1985) detected apsidal motion (precession of the periastron point) with a period of 10,750 years, which would imply a change in the value of ω1 of 0fdg76 during the ∼22.6 years that elapsed between their last observations (1985 October) and our first observations (2008 May). The actual measured change in ω1 is +0fdg39 ± 0fdg25. The predicted periastron precession is therefore not ruled out, but is not solidly confirmed either. With more extensive observations of V1143 Cyg, we hope to place more useful constraints on the magnitudes of the classical gravitational quadrupole and general relativity effects which cause the precession.

Figure 4.

Figure 4. RV measurements of the SB2 system V1143 Cygni.

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Table 6. Orbital Parameters and Stellar Mass Estimates for V1143 Cygni

Parameter Andersen et al. (1987) This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 7.64075217 ± 0.00000051 adopted from Andersen adopted from Andersen
T (reduced HJD) 42212.76652 ± 0.00015 54598.1853 ± 0.0027 54598.1835 ± 0.0088
e 0.540 ± 0.003 0.5469 ± 0.0010 0.5484 ± 0.0032
ω1 (deg) 48.6 ± 0.02 48.99 ± 0.25 48.84 ± 0.83
K1 (km s−1) 88.20 ± 0.20 88.867 ± 0.248 89.055 ± 0.836
K2 (km s−1) 91.10 ± 0.40 91.267 ± 0.311 91.508 ± 0.941
V0 (km s−1) −16.5 ± 0.7 −16.505 ± 0.074 −16.461 ± 0.235
Nobs 62    7    7
χ2 primary ...    63.01    5.98
χ2 secondary ...    46.49    5.04
σRV primary (km s−1) 1.1    0.734    0.789
σRV secondary (km s−1) 2.2    1.012    0.951
M1 (M) 1.391 ± 0.016 1.3815 ± 0.0114 1.3868 ± 0.0334
M2 (M) 1.347 ± 0.013 1.3451 ± 0.0100 1.3496 ± 0.0308

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Andersen et al. (1987) adopt an inclination angle of 87fdg0 ± 1° based upon eclipse photometry by Wood (1971), Popper & Etzel (1981), and van Hamme & Wilson (1984). Using that same value for i, we estimate M1 = 1.3815 ± 0.0114 M and M2 = 1.3451 ± 0.0100 M. The error bars on K1 and K2 dominate the error budget for the masses, so further high-accuracy spectroscopic observations of this system are clearly called for.

3.5. β Aurigae

β Aurigae (HR 2088, HD 40183, and HIP 28360) is another eclipsing double-lined binary, consisting of two A2 subgiants in a close four-day orbit. Smith (1948) measured the RV curves of both components, and Pourbaix (2000) reanalyzed these data in conjunction with interferometric astrometry data from Hummel et al. (1995) to refine the orbital parameters. Our RV curve is displayed in Figure 5. The phase coverage was insufficient to constrain e or ω1, so we assumed a circular orbit. Our derived parameters differ from the prior two analyses (Table 7), with K1 and K2 semi-amplitude values intermediate between those of Smith and those of Pourbaix. As with V1143 Cyg, this system exhibits a rotational line broadening of 30–40 km s−1, which increases the uncertainty of each RV measurement and thus the derived orbital parameters.

Figure 5.

Figure 5. RV measurements of the SB2 system β Aurigae.

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Table 7. Orbital Parameters and Stellar Mass Estimates for β Aurigae

Parameter Smith (1948) Pourbaix (2000)a This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 3.9600421 ± 0.0000013 3.96004 ± 0.00000267 adopted from Pourbaix adopted from Pourbaix
T (reduced HJD) 31076.719 43915.7 54539.0162 ± 0.0003 54537.0362 ± 0.0004
e 0.0 2.75266 × 10−6 ± 0.007 0.0 assumed 0.0 assumed
ω1 (deg) 0.0 139.043 ± 360.0 ... ...
K1 (km s−1) 107.46 ± 0.39 110.246 ± 1 108.053 ± 0.072 108.053 ± 0.099
K2 (km s−1) 111.49 ± 0.37 110.52 ± 2.1 110.911 ± 0.071 110.911 ± 0.098
V0 (km s−1) −17.06 ± 0.27 −15.7536 ± 0.62 −17.552 ± 0.037 −17.552 ± 0.052
Nobs 21 21     20    20
χ2 primary ... ...     54.19    28.30
χ2 secondary ... ...     40.83    21.15
σRV primary (km s−1) ... 2.740     0.363    0.363
σRV secondary (km s−1) ... 6.369     0.358    0.358
M1 (M) ... 2.4 ± 0.1 2.3885 ± 0.0129 2.3885 ± 0.0134
M2 (M) ... 2.44 ± 0.073 2.3270 ± 0.0126 2.3270 ± 0.0130

Note. aThese orbital parameters are listed in the downloadable data table at the SB9 Web site (http://sb9.astro.ulb.ac.be/mainform.cgi) but cannot be accessed directly from the Web interface.

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Adopting i = 76fdg0 ± 0fdg4 from Hummel et al. (1995), we calculate M1 = 2.3885 ± 0.0134 M and M2 = 2.3270 ± 0.0130 M. (Pourbaix uses i = 75fdg0 ± 0fdg73; the source of this value is unclear.) The majority of the 0.54% relative error in our mass values is due to the inclination angle uncertainty, so this system would be a prime follow-up target for further long-baseline spatial interferometry.

3.6. Mizar A

The brighter component of the visual binary Mizar (HR 5054, HD 116656, and HIP 65378) is itself a spectroscopic binary, with two early-A dwarfs in an elliptical 20 day orbit. Table 8 lists the orbital parameters measured by Fehrenbach & Prevot (1961) and the subsequent revisions computed by Pourbaix (2000) with astrometry data from Hummel et al. (1998), along with the values computed from our RV data (Figure 6). We find smaller velocity amplitudes and a slightly larger eccentricity for this binary system than prior researchers. Like the prior two targets, Mizar A's component spectra are moderately rotationally broadened, reducing the quality of the RV measurements.

Figure 6.

Figure 6. RV measurements of the SB2 system Mizar.

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Table 8. Orbital Parameters and Stellar Mass Estimates for Mizar A

Parameter Fehrenbach & Prevot (1961) Pourbaix (2000)a This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 20.5386 20.5385 ± 0.00013514 adopted from Pourbaix adopted from Pourbaix
T (reduced HJD) 36997.212 ± 0.022 38085.7 ± 0.0269224 54536.9882 ± 0.0068 54536.9904 ± 0.0106
e 0.537 ± 0.004 0.529404 ± 0.0052 0.5415 ± 0.0010 0.5415 ± 0.0016
ω1 (deg) 104.16 ± 1.15 105.5 ± 0.79 105.21 ± 0.14 105.27 ± 0.23
K1 (km s−1) 68.80 ± 0.79 67.2586 ± 0.96 66.479 ± 0.095 66.478 ± 0.153
K2 (km s−1) 67.60 ± 0.91 69.1796 ± 0.77 66.012 ± 0.118 66.019 ± 0.177
V0 (km s−1) −5.64 ± 0.15 −6.3077 ± 0.38 −7.342 ± 0.052 −7.309 ± 0.081
Nobs    15 15      18    18
χ2 primary    ... ...      82.55    33.70
χ2 secondary    ... ...      81.44    34.01
σRV primary (km s−1)    1.87 1.88094     0.556    0.566
σRV secondary (km s−1)    1.32 2.39922     0.641    0.638
M1 (M)    ... 2.5 ± 0.11 2.2224 ± 0.0221 2.2228 ± 0.0250
M2 (M)    ... 2.5 ± 0.12 2.2381 ± 0.0219 2.2383 ± 0.0246

Note. aWith some values from the SB9 catalog (Pourbaix et al. 2004).

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According to Hummel et al., i = 60fdg5 ± 0fdg3 for this binary. Using this value, we determine that M1 = 2.2224 ± 0.0221 M and M2 = 2.2381 ± 0.0219 M, for a relative mass error of 1.00% and 0.98%, respectively. The uncertainty in i is responsible for most of the mass error; if σi could be reduced to 0fdg05 and the errors on K1 and K2 could be cut in half, then the mass uncertainty would drop below 0.25%.

4. RESULTS FOR TRIPLE SYSTEMS

4.1. κ Pegasi

The κ Pegasi system (HR 8315, HD 206901, and HIP 107354) is a hierarchical triple, with two bright components (A and B) in an 11.5 year orbit, and a fainter unseen component in a six-day orbit around the B component. The canonical published orbit for this system comes from Mayor & Mazeh (1987), with more recent observations by Konacki (2005) (with orbit analyses published in Muterspaugh et al. 2006 and Muterspaugh et al. 2008) and our dFTS1 prototype (Hajian et al. 2007). Table 9 displays the orbital parameters as measured by Mayor & Mazeh, dFTS1, and dFTS2. Following Mayor & Mazeh, we assume that e = 0 for the short-period orbit. The dFTS2 observations of this system were made during two observing runs separated by ∼0.64 years, so we expect the V0 value of the short-period binary to change due to the long-period orbit. To account for this change, we treated the data from the two observing runs completely separately, and the results are given in two separate columns in the table. For the RV plot in Figure 7, we shifted Bb component's RV values from the first observing run by −1.198 km s−1 so that the two different epochs would share the same V0.

Figure 7.

Figure 7. RV measurements of the double-lined triple system κ Pegasi. Filled symbols denote the primary of the short-period pair (Ba), while open symbols denote the "A" component of the long-period orbit.

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Table 9. Orbital Parameters for the Single-lined B Component of κ Pegasi

Parameter Mayor & Mazeh (1987) Hajian et al. (2007) Muterspaugh et al. (2008) This Work (2007 Oct) This Work (2008 June)
P (days) 5.97164 ± 0.00006 adopted from M&M 5.9714971 ± 0.0000013 adopted from M&M adopted from M&M
T (reduced HJD) 44801.589 ± 0.015 53681.86 ± 0.04 52402.22 ± 0.10 54400.2125 ± 0.0005 54633.0989 ± 0.0005
e    0 adopted from M&M 0.0073 ± 0.0013 adopted from M&M adopted from M&M
K1 (km s−1) 42.1 ± 0.3 41.572 ± 0.257 ... 42.301 ± 0.025 42.527 ± 0.037
V0 (km s−1) −0.8 ± 0.2    ... −9.40 ± 0.22 −12.135 ± 0.016 −13.333 ± 0.022
VA (km s−1)    ...    ... ... 1.352 ± 0.851 2.019 ± 1.876
Nobs    30    9 30    7     4
σRV B (km s−1)    1.1    0.990 0.035    0.063     0.093
σRV A (km s−1)    ...    ... 0.250    2.084    3.249

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With only four RV measurements in the second observing run, the value for the K1 amplitude should be considered provisional, but the change in V0 is quite clear. We see an even larger change in V0 as compared to the mid-1981 observations of Mayor & Mazeh, although differences in RV zero point must be considered. Unfortunately, our prior dFTS1 observations did not yield a value of V0, because the template spectra were not referenced to an absolute wavelength standard.

RV measurements of the A component are not as precise as those of the B component, because its lines are much broader: we estimate vsin i = 47.9 km s−1 for A and 7.1 km s−1 for B. Even taking this fact into account, however, we find a much larger scatter of our RV measurements for A than expected from χ2 statistics. One possible explanation for this discrepancy is that the A component is also a close binary, as proposed by Beardsley & King (1976). We phased our RV data to their claimed 4.77 day period, but did not find any coherent cyclic pattern in the A component velocities. (Muterspaugh et al. 2006 see no evidence for a fourth component either.) The binarity of A is a possibility that we might explore with future data, but for the time being, this hypothesis is not supported.

4.2. η Virginis

The η Virginis triple system (HR 4689, HD 107259, and HIP 60129) was studied extensively by Hartkopf et al. (1992) who combined spectroscopy and speckle interferometry to determine the orbits of both the short-period (72 day) pair and the long-period (13.1 year) grouping. Hummel et al. (2003) made additional observations of this system with the NPOI interferometer, refining the orbital parameters and determining the inclination angle of the close binary orbit. Table 10 compares their parameters for the short-period Aa–Ab pair to our derivation. The parameters are in general agreement, except that the change in V0 is larger than previously seen, and is likely due to the gravitational influence of the third component of the system. Figure 8 shows the RV curves for the close binary, as measured by dFTS2. Note that the residuals for the secondary RV points all lie above the dotted line denoting zero residual. This offset may indicate a significant difference in the gravitational redshift or convective blueshift between the two component stars, or it may be an effect of the third component. Interestingly, Hartkopf et al. see a similar effect, but with the opposite sign, in that the V0 that they derive from the Aa RV curve is ∼0.4 km s−1 larger than V0 from the Ab component.

Figure 8.

Figure 8. RV measurements of the double-lined triple system η Virginis.

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Table 10. Orbital Parameters and Stellar Mass Estimates for η Virginis Aa–Ab

Parameter Hartkopf et al. (1992) Hummel et al. (2003) This Work (Formal RV Errors) This Work (Scaled RV Errors)
P (days) 71.7919 ± 0.0009 71.7916 ± 0.0006 adopted from Hartkopf et al. adopted from Hartkopf et al.
T (reduced HJD) 47583.98 ± 0.25 52321.4 ± 0.3 54403.7295 ± 0.0938 54403.6116 ± 0.3406
e 0.272 ± 0.009 (Aa) 0.244 ± 0.007 0.2518 ± 0.0011 0.2519 ± 0.0040
  0.258 ± 0.012 (Ab)      
ω1 (deg) 200.9 ± 1.5 196.9 ± 1.8 197.96 ± 0.48 197.21 ± 1.74
K1 (km s−1) 26.67 ± 0.20 Same as Hartkopf et al. 26.532 ± 0.054 26.606 ± 0.198
K2 (km s−1) 35.58 ± 0.31 Same as Hartkopf et al. 35.128 ± 0.081 35.236 ± 0.273
V0 (km s−1) 5.24 ± 0.19 (Aa) 4.9 ± 0.2 1.055 ± 0.009 1.118 ± 0.033
  4.85 ± 0.32 (Ab)      
Nobs 50  Same as Hartkopf et al.     11     11
χ2 primary ...  ...     292.62     25.75
χ2 secondary ...  ...     263.24     28.37
σRV primary (km s−1) 1.96  Same as Hartkopf et al.     0.129     0.150
σRV secondary (km s−1) 4.12  Same as Hartkopf et al.     0.231     0.218
M1 (M) 2.34 ± 0.2 2.68 ± 0.15 2.4818 ± 0.1158 2.5039 ± 0.1246
M2 (M) 1.95 ± 0.2a 2.04 ± 0.10 1.8745 ± 0.0874 1.8907 ± 0.0932

Note. aAssumed.

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Hartkopf et al. made a tentative spectroscopic detection of a blended Mg ii 4481 feature from the faint tertiary component, which appeared to be rotationally broadened by about 160 km s−1. Our instrument bandpass does not include this line, so we were unable to verify their detection, but we performed a crude three-dimensional cross-correlation using two narrow-lined template spectra plus a broad-lined A2V template. We found no evidence of a consistent RV solution for the third component.

According to the observations of Hummel et al. (2003), the inclination angle of η Vir Aa–Ab is 45fdg5 ± 0fdg9. Combining this number with our orbital parameters, we determine that M1 = 2.4818 ± 0.1158 M and M2 = 1.8745 ± 0.0874 M. The inclination uncertainty is the dominant contributor to the error budget, although the velocimetry results can certainly be improved with more data points.

5. SUMMARY

Our results demonstrate that dFTS technology is well suited to high-accuracy RV measurements of double-lined spectroscopic systems. We have determined the orbital parameters of six binary systems, matching or improving the published values for the masses of the component stars. We also observed two double-lined triple systems, providing some constraints on the nature of their stars.

For our future observational programs for spectroscopic binary stars, we are motivated by an assortment of specific scientific goals for which the capabilities of a dFTS are particularly applicable.

  • 1.  
    The most immediate goal is to continue to improve the accuracy of orbital parameters of binary systems, particularly the K amplitudes, and thus measure stellar masses more accurately. These advancements in spectroscopic capabilities must proceed in parallel with better astrometric measurements, as determined by current and future long-baseline spatial interferometers.
  • 2.  
    With high-accuracy RV measurements spanning longer periods of time, we will be able to detect and quantify secular changes in binaries' systemic velocities (V0) due to tertiary companions. As discussed by Tokovinin et al. (2006), the presence of a tertiary companion has significant implications for the formation of close binaries.
  • 3.  
    Observations of near-circular binary orbits will confirm or refute small non-zero eccentricities, thus providing observational validation for theories of tidal circularization and the influence of external gravitational perturbations such as Kozai resonances.
  • 4.  
    For highly elliptical systems like V1143 Cyg, long-term observing programs can measure changes in periastron angle to test theories of apsidal precession due to classical and relativistic effects.
  • 5.  
    Because the instrumental profile of a dFTS is easy to calculate a priori from the delay sampling function, we can measure spectral line broadening very accurately, e.g., to determine the projected rotational velocities of stellar components and thus shed light on tidal spin-up/spin-down mechanisms.

This research was funded in part by ARH's NSERC Discovery Grant.

We are grateful to the day crew at Steward Observatory—Jeff Fearnow, Dave Harvey, Bob Peterson, Gary Rosenbaum, and Bill Wood—for their assistance with the transport and installation of dFTS2, and we thank telescope operators Geno Bechetti, Dennis Means, and Peter Milne for their expertise in operating the telescope on our behalf. We also express our appreciation to the Director of the Steward Observatory for granting us telescope time over an extended period.

We are greatly indebted to the skilled instrument builders in the USNO Machine Shop—Gary Wieder, Dave Smith, Tie Siemers, and John Evans—for fabricating all of the custom optomechanical elements of dFTS2, as well as the thermal enclosure. We also thank the USNO Astrometry Department for travel support and salary support during the initial stages of this observing program, and thanks also go to the USNO Time Services Division for lending us packing crates for shipment of our instrument to Kitt Peak.

This research has made use of the SIMBAD database, operated at CDS, Strasbourg, France; NASA's Astrophysics Data System; and the SB9 catalog of Pourbaix et al. (2004). Richard O. Gray is to be commended for making his SPECTRUM codes so easy to install and use. Thanks also go to Farnoud Kazemzadeh for a critical reading of the manuscript, and to Frank Fekel and David Ramm for useful email discussions regarding the finer points of Spectroscopic binary analysis.

Note added in proof. After this paper went to press, we were alerted to the work of Southworth et al. 2007 (A&A, 467, 1215), who used high-precision photometry to derive an inclination angle i = 76fdg80 ± 0fdg10 for the beta Aurigae system. Using this value, we compute alternative results for Table 7: M1 = 2.3644 ± 0.0045 M and M2 = 2.3035 ± 0.0044 M (formal RV errors) or M1 = 2.3644 ± 0.0055 M and M2 = 2.3035 ± 0.0055 M (scaled RV errors). The relative mass errors are thus 0.19% (formal) or 0.24% (scaled). We also overlooked the recent publication of Konacki et al. 2010 (ApJ, 719, 1293), who used a specialized iodine cell technique to achieve excellent radial velocity precision on ι Pegasi, ω Dra and 12 Bootis, yielding stellar mass values with relative error bars of 0.065%, 11%, and 0.2% respectively. We thank the authors of both papers who brought these references to our attention.

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10.1088/0004-6256/142/1/6