Press Release
Open Access
Issue
A&A
Volume 651, July 2021
Article Number A85
Number of page(s) 18
Section Catalogs and data
DOI https://doi.org/10.1051/0004-6361/202039856
Published online 22 July 2021

© A. Brunthaler et al. 2021

Licence Creative CommonsOpen Access article, published by EDP Sciences, under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Open Access funding provided by Max Planck Society.

1. Introduction

Stars with more than about ten solar masses dominate galactic ecosystems. Understanding the circumstances of their formation is one of the great challenges of modern astronomy. In recent years, our view of massive star-forming regions has been dramatically changed by Galactic plane surveys covering the infrared (e.g., Galactic Legacy Infrared Mid-Plane Survey Extraordinaire (GLIMPSE; Churchwell et al. 2009), MIPSGAL; Carey et al. 2009, Hi-GAL; Molinari et al. 2010; sub-)millimeter (e.g., APEX Telescope Large Area Survey of the Galaxy (ATLASGAL; Schuller et al. 2009; Csengeri et al. 2014), Bolocam Galactic Plane Survey (BGPS; Aguirre et al. 2011), JCMT Plane Survey (JPS; Moore et al. 2015; Eden et al. 2017), the Millimetre Astronomy Legacy Team 90 GHz (MALT90; Jackson et al. 2013); and radio wavelength ranges (e.g., the Multi-Array Galactic Plane Imaging Survey (MAGPIS; Becker 1990; becker1994), the Sino-German 6 cm survey (Han et al. 2015)1, the Coordinated Radio and Infrared Survey for High-Mass Star Formation (CORNISH; Hoare et al. 2012; Purcell et al. 2013), The H I, OH and Radio Recombination line survey of the Milky Way (THOR; Beuther et al. 2016; Wang et al. 2020), the Southern Galactic Plane Survey (McClure-Griffiths et al. 2005), the VLA Galactic Plane Survey (VGPS; Stil et al. 2006), the Canadian Galactic Plane Survey (Taylor et al. 2003), the H2O Southern Galactic Plane Survey (HOPS; Walsh et al. 2011), the Methanol Multibeam Survey (MMB; Green et al. 2009), the Galactic Ring Survey (GRS; Jackson et al. 2006)). These surveys allow us for the first time to study all the evolutionary stages of massive star formation (MSF) in an unbiased way (e.g., König et al. 2017; Elia et al. 2017; Urquhart et al. 2018).

With the exciting results of the submillimeter and far-infrared (FIR) surveys from the ground (ATLASGAL) and space (Hi-GAL), the massive and cold dust clumps from which massive clusters form are now being detected galaxy-wide. Complementary to these surveys, the centimeter studies using the VLA allow very powerful and comprehensive radio-wavelength surveys of the ionized and the molecular tracers of star formation in the Galactic plane. There have been a number of VLA surveys of the inner part of the first quadrant of the Galactic plane starting with the pioneering 20 cm (Becker 1990) and 6 cm surveys (Becker et al. 1994) that are now combined in the MAGPIS project2. More recently the CORNISH team have mapped the northern GLIMPSE region at 5 GHz with higher resolution and sensitivity than MAGPIS. CORNISH was tailored to specifically focus on identifying and parameterizing the ultra-compact (UC) H II region stage of MSF (e.g., Purcell et al. 2013; Kalcheva et al. 2018), although it has also been used to investigate the Galactic population of planetary nebulae (PNe; Irabor et al. 2018). These studies have identified many thousands of radio sources located towards the Galactic plane, and follow-up work has allowed many hundreds of Galactic radio sources to be identified and studied (e.g., Urquhart et al. 2013; Cesaroni et al. 2015; Kalcheva et al. 2018; Irabor et al. 2018). However, these interferometric snapshot surveys have been limited by the historically small bandwidths available (∼50 MHz) and sensitivity to emission on larger angular scales. These surveys have therefore been restricted to continuum studies of relatively compact structures (i.e., < 20″ for CORNISH) and are therefore unable to provide us with a global view of star formation in the Galaxy.

The scope of radio-wavelength Galactic plane surveys and of radio interferometry in general, has been vastly increased with the expansion of the VLA into the Karl G. Jansky Very Large Array, (JVLA3). The VLA expansion project, beginning in 2001, with Early Science programs starting in early 2010, replaced the 1970s electronic and digital hardware with state-of-the art technology (for a description, see Perley et al. 2011). The expansion provided, among other things, continuous frequency coverage from 1 to 50 GHz with receivers with much wider bandwidth and better noise performance (see Table 1 of Perley et al. 2011). With the Wideband Interferometric Digital ARchitecture (WIDAR) correlator several metrics of the array’s spectroscopy performance improved by orders of magnitude in terms of instantaneous frequency coverage and spectral resolution (see Table 2 of Perley et al. 2011). Finally, of key importance for large area surveys, the “dead time” between any two observations (e.g., with a change of position) was much reduced from the 20 s typical of the old VLA down to the slew and settling time of the antennas, allowing efficient mosaicking strategies. All this makes the new VLA an extremely sensitive and efficient survey instrument. This is especially true for projects that combine continuum and spectral line observations, which was realized early on by Menten (2007), who described a project that has essentially evolved into the GLOSTAR survey.

The GLOSTAR survey has been designed to address the limitation placed on these previous surveys using the vastly improved capabilities of the upgraded VLA. Our goal was to use the extremely wide-band (4–8 GHz) C-band receivers of the VLA for an unbiased survey to find and characterize star-forming regions in the Galaxy. All fields are observed in the most compact D configuration of the VLA with a resolution of ∼18″ to have good surface brightness sensitivity for extended structures and in the more extended B configuration that provides a ten times higher spatial resolution to investigate compact sources. The VLA data are then complemented by observations with the Effelsberg 100-m telescope to provide zero spacings for the D-configuration data. Finally, the data from the D and B configurations are combined (D+B) to provide the best possible images of sources with intermediate sizes by combining the surface brightness sensitivity of the D configuration with the high resolution of the B configuration.

This survey of the Galactic plane detects tell-tale tracers of star formation: compact, ultra-compact, and hyper-compact H II regions and molecular masers that trace different stages of early stellar evolution and pinpoints the very centers of the early phase of star-forming activity. Combined with the submillimeter and infrared surveys, and our ongoing work in the Bar and Spiral Structure Legacy (BeSSeL) Survey4 to measure distances by trigonometric parallaxes to most of the dominant star-forming regions in the Galaxy, it offers a nearly complete census of the number, luminosities, and masses of massive star-forming clusters in a large range of evolutionary stages and provides a unique data set with true legacy value for a global perspective on star formation in our Galaxy. In addition to information on high-mass star formation, the GLOSTAR survey allows efficient identification and imaging of supernova remnants, planetary nebulae, and numerous extragalactic background sources.

2. The GLOSTAR VLA survey overview

2.1. Survey coverage

The full survey covers the Galactic plane in the range −2° < l < 60° and |b|< 1°, as well as the Cygnus X star-forming complex at a range of 76° < l < 83° and −1° < b < 2°, or 145 square degrees in total. We needed about 341 individual pointings to cover one square degree, or 49 463 pointings in total.

To date, the full survey region has been observed in the D configuration. For the higher-spatial-resolution observations in B configuration the region in the range 40° < l < 58° has not been observed yet. For the Galactic center region between −2° < l < 12°, we use the hybrid DnC and BnA configurations when possible, for which the northern arm of the array is in the more extended configuration to ensure a more circular synthesized beam. Since the hybrid configurations were not available after 2016, we use a combination of D and C configuration observations for the range 6° < l < 9°, and a combination of B and A configuration observations for l < 10° instead.

In this paper we show results and examples of the first 16 square degrees in the range 28° < l < 36° and |b|< 1°. The observations of this range were made under proposal code 13A-334 in the D and B configurations between 2013 April 6 and 2013 May 2, and 2013 September 29 and 2014 January 31, respectively.

2.2. Correlator setup

In GLOSTAR we observe two 1 GHz basebands in full polarization mode to measure the C-band continuum emission. Higher-frequency-resolution correlator windows are used to cover the most prominent methanol (CH3OH) maser emission line at 6.7 GHz (51–60 A+), seven radio recombination lines (RRLs) to study the kinematics of the ionized gas, and the 4.829 GHz (11, 0–11, 1) transition of formaldehyde H2CO, where absorption measurements can solve distance ambiguities. The lines are observed in dual polarization mode with channel spacings of 3.9 kHz for H2CO and CH3OH, and 62.5 kHz for the RRLs. The bands are centered at a local standard of rest (LSR) velocity of 50 km s−1. This setup avoids the strong persistent radio frequency interference (RFI) from a microwave link seen at 6.3 GHz at the VLA site, and allows for an estimation of the spectral index between the lower and higher basebands at 4.7 and 6.9 GHz, respectively. Table 1 lists the details of the setup used, together with the expected sensitivities for two scans with a total integration time of 15 s for each pointing. We note that the final sensitivities are expected to be at least a factor of two better, since each field is also covered by six neighboring fields. The continuum data is recorded with 16 spectral windows with 64 channels each, resulting in a bandwidth of 2 MHz for each channel. We use a correlator dump time of 2 s for all configurations. The high spectral and time resolution avoids any significant time and bandwidth smearing even when imaging the full primary beam. This setup results in a total data rate of 17.3 MB s−1.

Table 1.

Observed lines, bandwidth, number of channels and polarization products, channel spacings, velocity coverage, and theoretical sensitivity for two visits of one pointing (for the full 1 GHz for the continuum and 1 channel for spectral lines) of the VLA observations.

For the Galactic Center region from −2° < l < 2°, we use a slightly modified correlator setup, where we double the bandwidth of the spectral line observations at the cost of a lower velocity resolution. This was necessary due to the very broad velocity range seen in the Galactic Center.

In our first pilot observations in the range 58° < l < 60° we also used a different setup. Here the two continuum sub-bands covered the ranges 4.1−5.1 GHz and 5.9−6.9 GHz, and we had one additional high-resolution band covering the 6.035 GHz OH transition. However, due to very strong RFI at 6.3 GHz, we decided to change the frequency setup to avoid the strongest RFI.

2.3. Mosaicking strategy

The imaging of large regions on the sky with the VLA at medium radio frequencies (4–8 GHz) in a reasonable observing time requires very short scans per pointing. However, for short scans the overhead for slewing and settling of the antennas becomes an important factor for the total time estimate. On-the-fly mapping minimizes the overhead, but comes at the expense of highly increased data rates. If we move within a few seconds over one primary beam of the antennas, we have to sample the data with a short integration time of typically 0.5 s to avoid smearing effects. This results in a data rate exceeding 60 MB s−1, which is beyond the limit for regular VLA observations and much higher than the data rate of 17 MB s−1 that we use. Furthermore, we cannot time-average the data easily in post processing, which dramatically increases the required computing time. Therefore, we used traditional pointings over on-the-fly mapping.

Since the settling time of the VLA antennas is longer if the antennas move in azimuth compared to only elevation slews, we developed an observing scheme that minimizes the slews in azimuth. The CASA5 task makeschedule, which is now available as a contributed task6, can generate schedules that minimize the slew and settling times. Using this method we were able to get, on average, 7–8 s of good data from an observing scan of 11 s (i.e., an efficiency of ∼70%). In one five-hour observation, we mapped a 2° ×1° strip across the Galactic plane from |b|< 1° with typically 676 single pointings. Each pointing was observed twice for 11 s, yielding a total integration time of ∼15 s. The pointings were on a hexagonal grid with a grid spacing of θhex = 3.25′ (see Fig. 1 for an example). This corresponds to θB/2, where θB = 6.5′ is the primary beam at the central frequency of the higher continuum band (6.9 GHz). With this setup we have better than Nyquist sampling for most of the data, and also a better sampling than the θ B / 2 $ \theta_B/\sqrt2 $ used in other surveys, such as the National Radio Astronomy Observatory (NRAO) VLA Sky Survey (NVSS) (Condon et al. 1998) and CORNISH (Hoare et al. 2012). Having a denser grid has the advantage that the six neighboring pointings will contribute to the final image. Since neighboring rows are observed at different times, this will provide much better uv-coverage than a single pointing. The improved uv-coverage will be important for fields with strong and extended emission.

thumbnail Fig. 1.

Pointing configuration of a single observation spanning the range of 35° < l < 36° and |b|< 1°. The background image shows our D-configuration continuum data. Also shown are the primary beam sizes at the center frequency of the higher frequency continuum band (6.9 GHz) of one central pointing and its six neighboring pointings.

We used 3C 286 (and sometimes 3C 48 as a backup) as flux density and bandpass calibrator. A phase calibrator was observed every 15–20 min in D configuration and every 5–10 min in B configuration.

3. VLA data calibration

3.1. Continuum data

The continuum data were calibrated with the Obit package (Cotton 2008) using instrumental calibration signals and observations of celestial sources. The primary flux density and polarization calibrator was 3C 286 using the flux density scale of Perley & Butler (2013a) and the polarization of Perley & Butler (2013b). A secondary calibrator was chosen near the region being observed. Gain and delay calibrations were kept in a table and a single bandpass table was used. Flagging consisted of a list of data to be excluded and kept in a table. Calibration and editing consisted of the following steps:

  1. Convert from Archive format. The data were converted from archive format (ASDM/BDF) to AIPS format.

  2. Initial flagging. The flag table was initialized to the flags determined by the online system. Data were compared to running medians in time (each scan is at least three or four times the correlator dump time of 2 s) and frequency flagging the outliers. Antennas were flagged when shadowed by other antennas.

  3. Switched power calibration. An amplitude correction based on the switched power signal corrected for variations in system temperature.

  4. Parallactic angle correction. A time-dependent correction was applied to the calibration table for the parallactic angle of the antennas.

  5. Delay calibration. Group delay corrections were determined from calibrator data and applied to all sources.

  6. Bandpass calibration. Bandpass corrections were determined from the primary flux density calibrator 3C 286 using a model of the calibrator.

  7. Amplitude and Phase calibration. Gain solutions were determined for the amplitude and phase calibrators and were used to determine the spectrum of the phase calibrator that was then used to calibrate the target data. Solutions for 3C 286 used a structural and spectral model and were forced to the spectrum of Perley & Butler (2013a).

  8. Post calibration flagging. Another editing pass was done comparing the data with a running mean in frequency.

  9. Rinse and repeat. The solutions from the various calibration steps were compared with median values and outliers flagged, in the solutions and in the accumulated flag table. After the first calibration pass the calibration tables were deleted, the flag table was kept, and the calibration was repeated. This ensures that the calibration used well-edited data.

  10. Cross-hand delay calibration. The polarized calibrator, 3C 286, was used to determine cross-hand delay residuals.

  11. Instrumental polarization calibration. The polarization state of the secondary calibrator and the instrumental polarization were determined using observations over a range of parallactic angle.

  12. Cross-hand phase calibration. A cross-hand residual phase spectrum was determined from data on the polarized calibrator 3C 286 and the polarization model of Perley & Butler (2013b). This corrects the polarization angle on the sky.

3.2. Spectral line data

For the spectral line data we used a modified version of the VLA scripted pipeline7 (version 1.3.8) for CASA (version 4.6.0) that has been adapted to work with spectral line data. The calibration pipeline applies preliminary flags, such as flagging data that is not on source, shadowed antennas, and 5 % of the channels at both ends of a given sub-band, as these have low signal-to-noise ratios. It determines the absolute flux calibration and derives the delay, bandpass, and gain calibrations. In the default mode, it also automatically flags RFI using the RFI flagging algorithm rflag. The following modifications were made following the recommendations from the NRAO: no Hanning smoothing was performed in order to preserve the spectral resolution, the rflag flagging command was only applied to the calibration scans as it can often flag the spectral lines we want to observe, and statistical weights were not calculated as this sometimes affects bright sources, which is a concern for very strong masers. For the pilot region covered in this paper, the complex gain calibrator used was J1804+0101 and the flux calibrators were 3C 286 and 3C 48, using the flux density scale of Perley & Butler (2013a). After an initial run of the calibration pipeline, we perform quality checks and manually flag erroneous data, and rerun the pipeline until satisfied.

4. VLA data imaging

4.1. Continuum data imaging

The imaging of the continuum data was done with the wide-band, wide-field imaging task MFImage in the software package Obit (Cotton 2008). Instead of a joint deconvolution of all pointings into a single image, we image each pointing individually and then combine the images into one large mosaic. For each pointing, we imaged a field of view of 8.4′, which corresponds to the full primary beam of the lower continuum band. Since often there are sources outside the primary beam, which are bright enough to affect the data, we also use outlier fields at the location of known sources. We place an outlier field at the location of sources that are within 24′ of the pointing center and have a peak intensity of more than 10 mJy beam−1. It is possible to use the NVSS catalog (Condon et al. 1998) to determine the locations of outlier fields. However, since the NVSS was observed at a lower frequency of 1.4 GHz, there might be sources that are weak in the NVSS, but much stronger at our frequencies. Hence, we first did a very shallow imaging run of the entire survey using outlier fields from the NVSS. These images were then used to generate a new catalog of bright sources at 6 GHz that was subsequently used for the outlier fields in the final imaging.

Using wide-band data (bandwidth synthesis) with adequate spectral resolution provides improved coverage of the u-v plane giving a higher dynamic range as long as the varying source brightness and instrumental response with frequency are adequately accounted for. Wide-band imaging in MFImage is accomplished by dividing the observed total band-pass into frequency bins that are narrow enough not to cause significant problems, which in this case correspond to a fractional bandwidth of 5%. A frequency variable taper and/or Briggs Robustness factor is needed to produce approximately the same resolution in each frequency bin. Deconvolution using CLEAN proceeds by forming a weighted combined image that is used to select pixels at which CLEAN components are determined. The flux density at each pixel in each frequency bin is recorded and used in the generation of residual images, and self-calibration and restoration of CLEAN components. When the CLEAN is complete, each frequency bin is restored using the components subtracted from it, and a pixel-by-pixel spectrum is fitted correcting for the frequency-dependent primary antenna pattern. Since GLOSTAR observations are part of a mosaic, the primary beam corrections are applied in the linear mosaic produced later.

The three-dimensional aspect of the imaging (the image is flat and the sky is curved) is dealt with using faceting (i.e., tiling the field with smaller images to approximate a curved surface). Each facet is reprojected onto a common grid on a common tangent plane that allows CLEANing all facets in parallel.

The snapshot imaging of GLOSTAR observations produces relatively high sidelobes even with the extended u-v coverage provided by bandwidth synthesis. Therefore, restricting the CLEAN support region is important. The CLEAN window in which components are allowed is automatically adjusted from the statistics of pixel fluxes in each facet in each major cycle, and new portions of the CLEAN window are added as needed.

Radio continuum emission in the Galactic plane has structures on a wide variety of scales; the classical deconvolution into delta-function variant of CLEAN is inadequate. A multi-resolution CLEAN is implemented by generating a set of facet images in each major CLEAN cycle using a set of tapers resulting in a set of resolutions. In each major cycle a decision is made as to which resolution is to be CLEANed. The resultant point or Gaussian components are subtracted from the visibility data and a new set of residual images are generated for the next major cycle. In order to prevent CLEANing too deeply at a given resolution, the depth of each major cycle is restricted8. Atmospheric phase fluctuations can reduce the dynamic range in pointings with bright emission. A set of phase self-calibrations is triggered if the CLEAN results in a maximum image flux density in excess of a given threshold. A subsequent amplitude and phase self-calibration is triggered by a second threshold.

The maximum sensitivity can be obtained by a weighted combination of the overlapping observed pointing images onto a set of images covering the surveyed region. All else being equal, weighting by the square of the antenna power pattern in a given direction gives the optimum sensitivity. The mosaic formation process for each image plane is given by the summation over overlapping pointing images:

M ( x , y ) = i = 1 n A i ( x , y ) I i ( x , y ) i = 1 n A i 2 ( x , y ) . $$ \begin{aligned} M(x,{ y}) = {{\sum _{i=1}^{n}A_{i}(x,{ y})\ I^*_{i}(x,{ y})}\over {\sum _{i=1}^{n}A^2_{i}(x,{ y})}}. \end{aligned} $$(1)

Here Ai(x, y) is the antenna gain of pointing i in direction (x, y) and I i * (x,y) $ I^*_{i}(x,{\it y}) $ is the pointing i observed pixel value interpolated to direction (x, y) that was multiplied with the antenna gain in the observation and M is the mosaicked image. After combination, the spectrum in each pixel is redetermined.

4.1.1. D configuration

The complex and bright emission in the Galactic plane on various different scales is a challenge, in particular for snapshot observations. However, the use of two observations separated by a few hours and the large bandwidth of the observations greatly improve the uv-coverage, even if there are only ∼15 s of data per pointing. Since the D configuration observations are sensitive to scales up to 4′, we used multi-scale cleaning with three different scales: a delta function and scales of 20 and 40 times the cell size of the images, respectively. The cell sizes of the individual images were determined from the uv-coverage of the individual pointings and were typically about 2″. Cleaning was done down to a threshold of 0.25 mJy beam−1 and a maximum of 2000 iterations.

The individual pointings were all imaged using their intrinsic beam corresponding to the uv-coverage and weighting used. Hence, the beam sizes are slightly different for each pointing. Before combining all the pointings into one large mosaic covering the entire pilot region, we convolved all the pointings to a circular beam of 18″.

4.1.2. B configuration

For the B-configuration data we faced different challenges. Since we imaged the same primary beam at about ten times the resolution, the size of the individual images increased by a factor of 100, resulting in much slower processing. While most of the large-scale emission in the Galactic plane is resolved out in the higher resolution images, we found many artifacts from sources that are just seen on the shortest baselines of the B configuration (corresponding to ∼30″). Since there are only a few baselines that can see these extended sources, there is not enough data to image them. Hence, we restricted the uv-range to baselines of more than 50 k-λ, which resulted in much cleaner images and fewer artifacts. While there will always be sources that are visible just on the shortest baselines, the size distributions of the sources in our survey show that the number of sources drops significantly above a size of 30″ (Medina et al. 2019). Since the overwhelming majority of sources in the resulting images are now very compact, there is no need for multi-scale cleaning. The B configuration images are much less complex than the lower resolution maps. Therefore, it was possible to reduce the number of clean iterations to 250 per pointing. The threshold for cleaning was also 0.25 mJy beam−1, and the cell sizes in the images were 0.2″.

The individual pointings were again imaged using their intrinsic beam corresponding to the uv-coverage and weighting used. Hence, the beam sizes are slightly different for each pointing. Since the images of the B-configuration data have about 100 times more pixels than the D-configuration images, it was not practical to combine all the pointings of the pilot region into a single mosaic. As a compromise, we combined pointings into eight 2° ×1° strips across the Galactic plane (roughly corresponding to the individual observations, but also including pointings from the edges from the neighboring observations). Before combining the pointings they were convolved to a circular beam of 1.5″.

4.1.3. Combination of D and B configurations

There is a significant overlap in the baselines between the D configuration (35 m–1030 m) and the B configuration (210 m–11 100 m). Hence, it is possible to combine the two data sets and image them together. The uv-coverage for a single high-declination source from the D- and B-configuration data are shown in Fig 2. The resulting images have a reasonably good sensitivity to extended structures, but still a much higher resolution than only the D configuration images. While adding data from the intermediate C configuration with baselines between 35 m and 3400 m would be better, the additional observing time is difficult to justify.

thumbnail Fig. 2.

uv-coverage of a single source at high declination from the D configuration (left) and B configuration (right) observations. While both configurations probe very different ranges, there is significant overlap in the center that allows the combination into a single image. Part of this overlap is due to the large bandwidth covered by the observations.

The combination of D- and B-configuration data is the most time consuming since it still requires a large number of pixels and multi-scale cleaning. Since the range of different scales is even larger than in the D configuration images, we now allow for four different scales: a delta function, and scales of 20, 50, and 100 times the pixel size of 0.5″. A test with more scales made the imaging even slower, but did not change the final image significantly. The maximum number of iterations and the clean threshold were set to 2000 and 0.25 mJy beam−1, respectively. Before combining the pointings they were convolved to a circular beam. Since these combined images are mainly useful for structures with intermediate sizes, we used a beam of 4″ for the convolution.

4.1.4. Astrometric accuracy

As already discussed in Medina et al. (2019), the astrometric accuracy of the D-configuration observations is about 2″. For the B-configuration observations, Ortiz-León et al. (2021) estimated position errors of < 0.2″ by comparing methanol maser positions in the Cygnus X region with known positions from VLBI observations from Rygl et al. (2012). A more detailed discussion about the astrometric accuracy of the B-configuration data will be presented in forthcoming publications with the catalogs of these data.

4.2. Spectral line data imaging

4.2.1. Dirty image

Once the calibration, RFI removal, and continuum subtraction is complete, we move onto the imaging and source finding stage. This is done using the CASA software; one of the main reasons it is preferred over other software is due to its mosaicking task that can do joint deconvolutions of different fields.

We first produce what we call a “dirty” image of the D-configuration data, which is essentially the brightness distribution convolved with what is called the synthesized–dirty beam or point spread function (PSF). This image uses only the sampled visibilities and cannot recreate the entire sky brightness distribution without reconstruction techniques. These techniques are implemented via the CLEAN algorithm. Ideally, we would run the CLEAN algorithm over the entire data cube; however, for a 1° ×1° cube spanning at least 1000 channels, this can take around 3 weeks to complete. We opt instead to produce these dirty images, which take around 2 days for a cube of the same size.

In CASA the tclean task is implemented for the imaging of the dirty image with the following parameters: niter=0, since we do not deconvolve the image as we are not performing a full CLEAN at the moment; cube size (imsize) of 2500 × 2500 pixels, and pixel size (cell) of 2.5″. The number of channels (channels) and the rest frequency (restfreq) are set dependent on the transition. The weighting parameter is set to “natural” to better capture weaker sources; natural weighting has the best sensitivity, while “uniform” weighting gives better resolution.

The 1σ rms noise in the line free channels of the dirty cubes is found to be ∼20 mJy beam−1, which is consistent with the noise estimated using the VLA Exposure Calculator for both the methanol and formaldehyde lines. We note that the expected noise level for a total of 15 s integration time in the D configuration with a channel width of ∼3.9 kHz is actually ∼40 mJy beam−1, but since each field is covered by six neighboring fields the final sensitivities will be at least a factor of two better (∼20 mJy beam−1), as mentioned before.

We find that weak and isolated masers can be detected already from the dirty image, meaning that it is not necessary to CLEAN the entire image. Only weak masers that are in the vicinity of strong masers in both the spatial and velocity domains can possibly be missed. It is thus much more efficient to search for these dirty cubes first and compile a preliminary catalog of detections. The next step is to cut out smaller regions encompassing the detections and CLEAN them to search for weaker detections that were in the vicinity of stronger detections. A detailed description of the source finding algorithm for the masers that was used to find the sources will be included in an upcoming paper (Nguyen et al., in prep.).

4.2.2. Final CLEAN

Patches of 0.23° ×0.23° using on average 16 pointings centered on the sources detected in the dirty images were split out to make smaller visibility data sets for CLEANing. The cell size and/or pixel size was retained at 2.5″ for the D configuration, and the imaging was restricted to the velocity ranges over which a significant signal was detected. This produced images with spatial extents of 350 × 350 pixels and spectral extents of ∼18–25 km s−1 centered on the peak velocity. A CLEANing threshold of 60 mJy beam−1 was chosen (∼3σ) and the parameter niter (number of minor CLEAN cycles) was set to 1000, 5000, or 10 000 depending on the strength of the maser involved, with niter = 1000 to CLEAN patches containing weak masers to niter = 10 000 for patches containing very strong sources. These iteration values were found to optimize the automatic cleaning for many sources to maximize image fidelity while avoiding overcleaning. The weighting parameter was set to uniform since it gives a better resolution, thus giving better positional accuracy of the source.

Additionally, B configuration images were also produced for the methanol maser data. With a higher angular resolution of ∼1″, to image and CLEAN an area of similar size to the D-configuration data would take significantly more time. However, thanks to the benefit of first studying the D-configuration data, we made smaller images (0.1°   ×  0.1°) using the B-configuration data centered on detected features from the D-configuration data, thereby efficiently using our available computing resources. We used a pixel size of 0.3″, resulting in images with spatial extents of 1200 × 1200 pixels and similar spectral extents to those above. Similar CLEANing iteration parameters were used depending on the individual source intensity.

4.2.3. Radio recombination line imaging

To increase the signal-to-noise ratio of RRL emission, we observed multiple RRLs with the goal to stack them in velocity. We observed seven RRLs (Table 1), which were chosen to avoid radio frequency interference (RFI) and due to bandwidth limitations. We inspected the calibrated data for RFI with automatic tools, such as rflag in CASA, and manually, and flagged data that were corrupted. Since we found that the H96α line is strongly affected by RFI, we decided to exclude this transition in the following.

The lines were imaged individually in fields with dimensions Δl = 1° and Δb = 2°. We included in the imaging pointings from adjacent scheduling blocks to provide uniform sensitivity across the edges of the images, and to include sources whose sidelobes may significantly affect the image quality and need to be accounted for during the imaging process. We subtracted the continuum in the uv-domain from line-free channels, which are selected from uniform line-free velocity ranges. The data were imaged and deconvolved with a threshold of several times the noise level using tclean in CASA (version 5.7.0), with the sub-parameters imagermode=“mosaic” and gridder=“mosaic”. By setting restoringbeam=“common” the residuals of all channels in a spectral cube were subsequently smoothed and the image restored with a common beam. The original bands span 8 MHz with 128 channels, yielding a velocity resolution of 2–4 km s−1 (see Table 1). The images were gridded in velocity bins of 5 km s−1 with a velocity range from −150 km s−1 to 150 km s−1.

In this paper we show the RRL emission for two regions, the massive star-forming region G29.92−0.03, also known as W43-south, and the H II region G28.60−0.37. To optimize imaging and angular resolution, the data were re-imaged for these objects in two cubes with dimensions of Δl = 0.2° and Δb = 0.2°, and all lines smoothed to an angular resolution of 25″ before stacking. The images were rotated into Galactic coordinates. The noise levels of the smoothed images are in the range 5–10 mJy beam−1 with the noise of the stacked images of ∼3 mJy beam−1 at an average frequency of 5.3 GHz. A full description of the RRL data will be given in a forthcoming publication.

5. Effelsberg observations and imaging

5.1. Observations

The GLOSTAR single-dish observations of the pilot region were performed with the 100-m telescope at Effelsberg, Germany9, from 2019 January to September. We used the S45mm receiver installed at the secondary focus as front end. The S45mm receiver is a 4.5 cm broadband receiver with two orthogonal linear polarizations. We simultaneously employed two different kinds of back ends: SPEctro-POLarimeter (SPECPOL) and fast Fourier transform spectrometers (FFTSs: Klein et al. 2012). SPECPOL is used to obtain the Stokes parameters (I, Q, U, V). SPECPOL delivers two bands covering 4–6 GHz and 6–8 GHz. Each band provides 1024 channels, resulting in a channel width of 1.95 MHz. The phase shifts between different channels in Stokes parameters were fixed by the ADC synchronization procedure before our survey observing sessions. FFTSs deliver two low spectral resolution bands and two high spectral resolution bands that are used for spectral studies. The two low spectral resolution bands cover 4–6.5 GHz and 5.5–8 GHz. Each band provides 65536 channels, resulting in a channel width of 38.1 kHz, corresponding to a velocity spacing of 2.2 km s−1 at 5.25 GHz. The two high spectral resolution bands are designed to study H2CO (11, 0–11, 1) and CH3OH (51–60 A+). These two bands have bandwidths of 200 MHz. Each band provides 65536 channels, resulting in a channel width of 3.1 kHz, corresponding to a velocity spacing of 0.14 km s−1 at 6.7 GHz (for a selection of the observed spectral lines, see Table 2).

Table 2.

Selection of spectral lines covered with the GLOSTAR Effelsberg observations.

The pilot region is divided into cells of 0.2° (l) × 2° (b) and 2° (l) × 0.2° (b). Each cell was observed in the on-the-fly (OTF) mode with a scanning speed of 90″ per second with a step of 30″ between OTF subscans in order to conform to the Nyquist sampling theorem. Each dump consists of two phases, for one of which the calibration signal is switched on. The sampling time is 125 ms for each phase. The pilot region was observed twice, along the Galactic longitude and latitude, in order to reduce the scanning effects and allow basket weaving (e.g., Winkel et al. 2012a).

Pointing and focus was checked on strong continuum sources at 6.7 GHz. NGC 7027 was used as flux calibrator, while 3C 286 was used as polarization calibrator. The half power beam width (HPBW) was 140″, at 5 GHz. The typical system temperature was 28–42 K. Almost all observations were carried out during the night to avoid the influence of the strong solar emission from the telescope sidelobes.

5.2. Calibration

The polarized calibrator 3C 286 was used to calibrate the flux density and polarization of our radio continuum data. Based on the Effelsberg long-term monitoring observations (A. Kraus, priv. comm.), the flux density of 3C 286 follows the relationship

log 10 ( S ν [ Jy ] ) = 1.11578 + 0.494671 × log 10 ν [ MHz ] 0.151995 × ( log 10 ν [ MHz ] ) 2 , $$ \begin{aligned}&\mathrm{log}_{10}(S_{\nu } [\mathrm{Jy}]) = 1.11578+ 0.494671\times \log _{10}\nu [\mathrm{MHz}]\nonumber \\&\qquad \qquad \qquad \qquad -0.151995\times (\mathrm{log}_{10}\nu [\mathrm{MHz}])^{2} , \end{aligned} $$(2)

and has a nearly constant linear polarized angle of 33° and a linear polarization degree of 11% at the observed frequencies (4–8 GHz). Based on these values, we obtained the Müller matrix by observing 3C 286 at different parallactic angles. The derived Müller matrix is then applied to our data in order to correct the instrumental effects of the receiver. In addition, the parallactic dependence of the polarization measurements are corrected.

Data reduction was carried out with the NOD3 software package (Müller et al. 2017). Strong RFI is present across the observed frequencies. Thanks to the newly installed SPECPOL, we were able to select specific frequencies while filtering out RFI-affected channels. This resulted in two continuum images centered at 4.8 GHz and 7.0 GHz, respectively. The remaining RFI was flagged by data editing in NOD3. For each subscan, a linear baseline is subtracted in order to correct gain drifts. For each field, the coverage scanned in the l and b directions were combined with the basket weaving technique, which significantly reduces the scanning effects and artifacts.

Since we only observed the Galactic plane within |b|≤1.0°, all maps have a relative zero-level shift due to the baseline subtraction. These zero-level shifts result in negative values in the reduced map (see Fig. 3a). Here we used the Sino-German 6 cm data from the Urumqi telescope (Sun et al. 2007, 2011) to restore the extended emission at 4.8 GHz because the effective center frequency is nearly identical. We first applied high cuts to both images to avoid the contamination from the convolution of strong compact sources that may spread emission to extended emission in the convolved images. The high cut value was set to be 15 K and 4 K for the Effelsberg and Urumqi images, respectively. We then convolved both images to an angular resolution of 15′ (see Fig. 3b), and obtained the difference of the two images (see Fig. 3c). In order to only restore the large-scale emission, we applied the background filtering method to the difference map (Sofue & Reich 1979). This method is used to avoid the contributions of the Urumqi data on small scales that can be affected by pointing errors and slightly deformed shapes of compact sources. We used a filtering beam size of 30′ and 50 iterations to decompose the difference map until the compact and extended emission are well separated (see Figs. 3d–e). Then the extended component of the difference map (Fig. 3d) was used to correct the zero-level shift in the original Effelsberg 4.8 GHz continuum data, which leads to the restored data set (see Fig. 3f). Since there is no available public data that can be used to correct the zero-level shift at 7 GHz, we derived the extended emission at 7 GHz using the data from the Effelsberg 11 cm survey (Reich et al. 1990) and the Urumqi 6 cm survey (Sun et al. 2007, 2011). These data were convolved to an angular resolution of 15′ in order to derive the spectral index of the extended emission. The 7 GHz extended emission was then calculated by interpolation with the derived spectral index. Similarly, we calculated the difference between the derived and observed 7 GHz data at a common angular resolution of 15′, and we used the same method to restore the extended emission at 7 GHz. We also note that the extended emission at 7 GHz is derived from the interpolation of images at only two frequencies. Thus, the uncertainties in the extended emission are greater in the 7 GHz continuum data than in the 4.8 GHz continuum data.

thumbnail Fig. 3.

Zero-level shift correction for the Effelsberg data. (a) Effelsberg 4.8 GHz continuum image. (b) Urumqi 6 cm continuum emission overlaid with the Effelsberg 4.8 GHz continuum contours. Both data sets have been convolved to an angular resolution of 15′. The contours start at 50 mK, and each contour is twice the previous one. (c) Difference map derived by subtracting the Urumqi 6 cm continuum emission from the Effelsberg 4.8 GHz continuum map in Fig. 3b. (d) Extended emission component of Fig. 3c derived by the background filter method. (e) Compact emission component derived by the background filter method. (f) Restored Effelsberg 4.8 GHz continuum image.

The calibration of the spectral line data follows the recipes described in Kraus (2009), with several improvements to account for the frequency dependence of receiver gain, system and noise diode temperatures and atmospheric effects (see Winkel et al. 2012b). In particular, atmospheric opacity is corrected for using a newly developed water vapor radiometer. For absolute flux calibration, we used spectroscopy pointings on the unpolarized calibrator NGC 7027 in comparison with a model. The two wide bands of 2.5 GHz were split into several sub-bands for calibration. The two 200 MHz narrow bands were calibrated independently. The spectra were converted to main beam temperature using a main beam efficiency of ηmb ∼ 0.65.

The frequency range 4–8 GHz contains a variety of spectral lines, all of which are simultaneously covered with the WFFTS back ends. We focused on a subset of these, which are very interesting for the study of the ISM and are likely to be detected. We note that not all of them are usable due to the contamination by artifacts such as RFI. An overview of the lines is given in Table 2, together with the native channel width and typical RFI contamination before any RFI removal. After calibration we subtracted a first-order baseline for each spectral line using line-free channels that are offset in velocity from the main Milky Way emission. The final mapping of each line was done in GILDAS10 with CLASS (Pety 2005). We used the standard gridding kernel of 1/3 of the beam size, which yields slightly lower angular resolution in the final images than the raw telescope beam. We grid the data from both longitude and latitude scans together. The noise levels vary across the maps due to different elevations and weather conditions. For molecular transitions, we resampled the final maps with channel widths close to the original resolution, while the actual velocity resolution was a factor of two coarser since the data was smoothed with a Gaussian kernel in the process of regridding to the LSR rest frame. For the RRLs, due to their broader intrinsic line widths and to obtain independent channels at all frequencies, we resampled all lines at 5 km s−1. Details of the data cubes of all gridded lines are given in Table 2. Given the wide bandwidth of the FFTS back ends, velocity coverage is continuous. We typically grid a wide enough velocity range to cover Galactic emission and to verify that the region for baseline subtraction is not affected by RFI. Stacking multiple RRLs in velocity further increases the signal-to-noise ratio. Using approximately seven RRLs without further flagging of RFI, smoothing all lines to a common angular resolution of 180 ″, and using the mean to combine the maps at each position and velocity channel yields an RMS of typically 0.008 K at 180″ resolution in a channel 5 km s−1 in width.

5.3. Combination of VLA and Effelsberg data

Combining the Effelsberg data and the VLA D-configuration continuum data is not straightforward, due to the different frequency coverages. While the VLA observations cover two 1 GHz bands, the Effelsberg observations include the full range from 4 to 8 GHz. Furthermore, the RFI situation at the two locations is very different. Hence, it is not possible to compute images averaged over frequency and then combine the two averaged images. Instead, we used the two images obtained from the Effelsberg data with frequency ranges of 4–6 GHz and 6–8 GHz and average frequencies of 4.8 GHz and 7 GHz, respectively. With the multi-frequency data from the VLA data, we generated two images corresponding to the same frequencies. Then we used the task Feather in Obit (Cotton 2017) to generate two combined images of VLA and Effelsberg at low and high frequencies. Finally, these two images were combined pixel-by-pixel to create the final image and a spectral index map. The combination of the spectral line data from the VLA and Effelsberg will be done in the future.

Comparing the flux scales between the Effelsberg and VLA observations is difficult due to the different spatial resolutions. The Effelsberg images obviously pick up more extended emission, which is filtered out by the VLA. However, the Effelsberg data and the Urumqi 6 cm data agree to within 2%, and the flux calibration of VLA observations is typically also good to at least 5%. Medina et al. (2019) found good agreement between the GLOSTAR and CORNISH/MAGPIS fluxes. To compare the scales, we smoothed the VLA image at 4.8 GHz to the beam size of the Effelsberg observations and then fitted Gaussians to several sources in the entire region that are relatively isolated (although there is always some diffuse emission in the Effelsberg images). The results are shown in Fig. 4. While some sources have higher Effelsberg fluxes, as expected if there is extended emission, there is no clear systematic offset between the two data sets. Hence, no flux scaling was performed before combining the images.

thumbnail Fig. 4.

Comparison of peak fluxes of several sources for the Effelsberg and VLA images. The solid line denotes a 1:1 ratio.

6. Results

The continuum and spectral line data at various resolutions allows us to address a large variety of different science cases. It would be well beyond the scope of this paper to discuss these in detail. Hence, this section gives only a small overview of some of the science that can be done with this data. This will be investigated in much more detail in forthcoming papers. We plan to release all continuum images (D+Effelsberg, D, D+B, and B) as well as continuum and spectral line source catalogs and spectra of the detected lines in the future on our survey website11.

6.1. Continuum

The full continuum image of the pilot region covering the range from 28° < l < 36° is shown in Fig. 5. Here we show the combined image using the VLA D configuration and the Effelsberg data (top) as well as the VLA-only image (bottom). As expected, the addition of the Effelsberg single-dish data helps to resolve many of the missing flux problems seen in the D configuration-only images. However, a few artifacts remain, mainly near very bright and compact sources.

thumbnail Fig. 5.

Radio continuum image of the pilot region in the range 28° < l < 36°. Top: combination of the VLA D configuration and the Effelsberg single-dish images. Bottom: D configuration VLA image of the full continuum of the same longitude range already shown in Medina et al. (2019).

In the D configuration image we find a total of 1575 discrete radio sources and 27 large-scale structures. From these sources, 231 continuum sources were classified as H II regions, 37 as ionization fronts, and 46 as planetary nebulae. The catalog of sources is published in Medina et al. (2019). In the B configuration images, we detect about 1400 sources above 7σ in total (Dzib et al., in prep.). The similar detection rate to the D configuration images can be explained by lower noise in regions with extended emission in the D configuration images, by sources that split into multiple sources at a higher spatial resolution, while extended sources are completely resolved out. In the same region the CORNISH survey with the same spatial resolution as our B configuration images finds a total of 353 sources (Purcell et al. 2013).

In addition to many sources that are located in the Milky Way, there is also a large number of extragalactic sources in the survey. While these sources were not the main focus of the survey, they are an interesting by-product (e.g., Chakraborty et al. 2020).

In Fig. 6 we show the details of a smaller region on all available scales, starting with the Effelsberg and D configuration combination down to the image using only the B configuration that contains only the most compact sources. While some of the extended emission is resolved out in the combined images, the higher resolution shows finer details of the sources.

thumbnail Fig. 6.

Comparison of a smaller region between the D configuration and Effelsberg combination (left), the D configuration only (middle left), the combination of D and B configurations (middle right), and the B configuration only (right).

6.1.1. Supernova remnant G28.78−0.44

Though the non-thermal emission is faint in C band compared to lower frequencies, the high sensitivity of the GLOSTAR survey data allows us to observe extended non-thermal emission quite well. All supernova remnants (SNRs) with previous radio observations present in the catalog of Galactic SNRs (Green 2019) were detected in the GLOSTAR data. Since SNRs are in general linearly polarized, the GLOSTAR polarization data are helpful in identifying new SNRs.

As an illustration, we present the GLOSTAR Stokes I and the linearly polarized emission ( Q 2 + U 2 $ \sqrt{Q^2 + U^2} $) of the MAGPIS candidate SNR G28.76−0.44 (Helfand et al. 2006) in Fig. 7. The linearly polarized flux density was measured in each channel first and then averaged in order to account for bandwidth depolarization effects. On the linearly polarized flux density map, we also show the electric field vectors corrected for rotation measure (RM). The RM was measured using a linear fit of polarization angle measured in each channel against λ2, where λ is the central wavelength of that channel. The mean RM in this region was −58 rad m−2 with uncertainties of 25−35 rad m−2.

thumbnail Fig. 7.

Continuum images of the supernova remnant G28.78−0.44 from the VLA D-configuration data in total intensity (left) and polarized intensity with electric field vectors (right).

We observe that the electric field vectors are preferentially aligned along the shell, implying that the magnetic field is pointing radially outward of the remnant. A radial magnetic field is typically observed in the shells of young SNRs (Milne 1987). This is likely due to the effect of magnetic field stretching caused by Rayleigh-Taylor instabilities in the turbulent layer between the ejecta and the ISM (Jun & Norman 1996). The detection of polarized emission now finally confirms that the source is indeed a supernova remnant. This object, along with several other candidate SNRs, is discussed in Dokara et al. (2021).

6.1.2. The hypercompact H II region G28.2−0.04 N

Hyper-compact H II (HC-H II) regions trace the earliest phases of massive star formation. At the GLOSTAR observed frequencies (∼6.0 GHz) the emission from them is expected to be optically thick, and with spectral indices of 1−2 (Kurtz 2005). Thus, they are expected to be relatively weak at these frequencies. The sensitivity provided by previous surveys bias the results and made HC H II regions difficult to detect (Kurtz 2005). The better sensitivity provided by GLOSTAR could partially alleviate this bias. Here, we present an example of a well-known HC H II region and its properties in the GLOSTAR images.

G28.2−0.04 N, shown in Fig. 8, was one of the first radio sources classified as a HC H II region given its properties at radio frequencies (e.g., broad radio recombination lines, rising spectral index, high electron density; Sewilo et al. 2004). It has been observed and detected in our GLOSTAR observations. However, the morphology in the final maps is different.

thumbnail Fig. 8.

From left to right: images from D, D+B, and B configurations of G28.2−0.04.

In the low-resolution image it is detected as a single source and with a total flux of 396 ± 20 mJy (labeled G028.200−00.050 in our catalog; Medina et al. 2019). On the other hand, in the combined map (VLA D+B) two sources are clearly spatially resolved. These two sources are the components of the system, G028.2−0.04 N and G028.2−0.04 S. The integrated fluxes of these sources are 210 ± 4 mJy and 132 ± 4 mJy. Finally, in the high-resolution map the northern component is circular, while the southern component is shapted like a shell. Their integrated fluxes are 147 ± 7 and 22 ± 1 mJy.

The in-band spectral index of the northern component is 0.8 ± 0.1, which is consistent within two sigma with earlier values of 1.0 ± 0.1 obtained by Sewilo et al. (2004). It is worth highlighting that the earlier estimates were obtained with dedicated observations in different bands.

6.2. 6.7 GHz methanol

The 6.7 GHz CH3OH maser was first discovered by Menten (1991) and is one of the brightest species of masers observed. It has already been shown to be exclusively associated with young massive stars (Minier et al. 2003; Xu et al. 2008), and therefore a sensitive and unbiased survey would trace the early stages of high-mass star formation in our Galaxy. Furthermore, the distribution of these masers can help us study the structure of the spiral arms within the Milky Way. While previous studies already exist, most notably the Methanol Multibeam (MMB) survey (Green et al. 2009) and other surveys (Pestalozzi et al. 2005; Pandian et al. 2007; Yang et al. 2019), our VLA data is the most sensitive (RMS ∼ 18 mJy beam−1), thus providing potentially the most complete catalog to date. In addition to the D configuration data, we also have B-configuration data for a large fraction of the survey in order to provide more accurate positions and observations of multiple epochs.

G35.197−0.753 (Xu et al. 2008; Breen et al. 2015) is an example source, and is shown in Fig 9. Plotted are peak intensity maps (PIMs) where we take the highest intensity along the velocity range and map it accordingly. From this figure, we can already see the benefit the additional higher resolution data provides as we are able to clearly differentiate two sources spatially. Inspecting the spectra, we also find that the brightest component seen in the D-configuration data at 28.51 km s−1 originates in the southern source, while the remaining velocity components belong only to the northern source.

thumbnail Fig. 9.

Peak intensity maps (PIM) over the velocity range of the methanol maser source G35.197−0.743 and spectra obtained from VLA data. On the left is the VLA D configuration data, which has an average beamsize of ∼18 arcsec. When observed in the B configuration (with beamsize ∼1.5 arcsec, middle panel), one can see that the higher resolution allows us to resolve the maser into two sources. Viewing the spectra on the right, we see that the first peak at 28.51 km s−1 belongs only to the southern source while the rest belong to the northern source. The white contours mark the GLOSTAR radio continuum emission.

Furthermore, our access to multiple epochs allows us to observe potential maser variability that is not yet well understood. Maser variability typically occurs with periods of ∼20 to 200 days and with sinusoidal patterns or intermittently with a quiescent phase (Goedhart et al. 2004; Szymczak et al. 2018; Olech et al. 2019). There are two kinds of models to explain the observed variability. The first explains the variation through cyclic variations in the seed photon flux from a colliding-wind binary (CWB; van der Walt et al. 2009, van der Walt 2011). The second type of model assumes changes in the temperature of the dust grains in the environment of the masing region. This affects the infrared radiation flux, and thus the pump rate. There are multiple hypotheses for the origins of the changes in the temperature, such as periodic accretion from a circumbinary accretion disk (Araya et al. 2010), stellar pulsation (Inayoshi et al. 2013; Sanna et al. 2015), and spiral shock waves in the disk of a binary system (Parfenov & Sobolev 2014; Szymczak et al. 2018).

We show in Fig. 10 the peak flux density of G30.851+0.122 of the two configurations and the MMB spectrum. Here we see that our sensitivity appears to be better by a factor of ∼10 compared to the MMB. We also see that in the GLOSTAR data, the first two velocity components match, while the third component decreases to roughly 60% over the course of 8 months (the time between observations of VLA D configuration and B configuration). The combination with other known surveys with GLOSTAR can give us an even broader glimpse into the nature of methanol maser variability.

thumbnail Fig. 10.

Methanol maser spectra of source G30.851+0.122. Shown are the GLOSTAR spectra in black and red solid lines for D configuration and B configuration, respectively. The dashed blue line is the MMB spectrum of the corresponding source. The right inset depicts a zoom-in of the velocity component, which shows a difference in intensity between the two configurations; it is spatially unresolved in D and in B configuration.

6.3. 4.8 GHz formaldehyde

It has been known for some time that H2CO is associated with massive star-forming regions. Furthermore, Downes et al. (1980) found that 80% of the H II regions surveyed had H2CO absorption. In particular, the 110 − 111 line of H2CO is mainly observed in absorption at 4.8 GHz and is associated with interstellar dust clouds against the 2.73 K cosmic microwave background (CMB) (Snyder et al. 1969). It has been found that these absorption features can be used to trace the kinematics of infrared dark clouds (IRDCs) and are associated with infrared sources (Okoh et al. 2014). Furthermore, H2CO is ubiquitous and is therefore a good probe of the physical conditions of molecular clouds with densities 103 − 105 cm−3 (Mangum & Wootten 1993), and thus the cold and dense molecular clouds.

We follow a procedure similar to our methanol analysis. The analysis of the pilot region resulted in a detection of 20 compact H2CO absorption sources. Compared with the catalogs of Downes et al. (1980) and Okoh et al. (2014), this corresponds to a detection rate of ∼40%. The strongest sources in their catalogs were all detected automatically from our source extraction, while three other sources were found after a manual inspection. The discrepancy can be explained from the much longer integration time used by previous surveys (> 15 min) that would allow them to detect many more weaker sources. Furthermore, their observations have resolutions of 2.6′ and 10′, respectively, which is a factor of 5–20 higher than ours. It is then plausible that some of these sources were resolved out due to our much higher angular resolution.

First detected by Downes & Wilson (1974), formaldehyde was also found to show maser emission at 4.8 GHz. However, despite dedicated attempts to detect these molecules again, formalehyde remains very rare and seem to be exclusively related to the high-mass star formation process. Within the pilot region, only the G32.744−0.076 H2CO maser (Araya et al. 2015) was detected, and is shown in Fig. 11, while the maser G29.96−0.02 reported by Pratap et al. (1994) was not detected.

thumbnail Fig. 11.

Formaldehyde maser in G32.744−0.076. Top: peak intensity map of known 4.8 GHz formaldehyde maser G32.744−0.076 (Araya et al. 2015) using GLOSTAR VLA D-configuration data and the continuum emission (white contours). Bottom: spectra extracted from GLOSTAR (solid black line) and from the Araya et al. (2015) paper (dashed red line). Despite the lower sensitivity of our data, the faint superimposed absorption feature can be seen.

6.4. Radio recombination lines

Radio recombination lines are tracers of ionized gas in H II regions and have been used to confirm H II region candidates detected in near-infrared emission (e.g., Anderson et al. 2014). They provide kinematic and therefore distance information, and allow us to study of physical properties of the emitting gas, such as the determination of the electron temperature (e.g., Quireza et al. 2006) and the feedback of H II regions on the surrounding molecular cloud environment. We highlight two examples of RRL emission detected with the GLOSTAR survey for its pilot region. The ∼100 RRL detections in the pilot region will be described in greater detail in forthcoming works. Here, we show an example of a relatively isolated region of star formation, G28.694−0.359, and possible interaction with the surrounding molecular gas. We show the different aspects that the GLOSTAR data tell us about high-mass star formation via the example of the massive star-forming complex G29.93−0.03.

6.4.1. H II region G28.594−0.359

The H II region G28.594−0.359 shows two lobes that are resolved in the GLOSTAR B+D configuration continuum data (Fig. 12). The RRLs indicate a LSR velocity of 90 km s−1. Using the parallax-based distance calculator from Reid et al. (2016), we get a distance of 4.5 ± 0.4 kpc. The ATLASGAL 870 μm sources associated with the H II region show similar distances of 4.7–4.8 kpc (Urquhart et al. 2018). The lobes have a radius of 0.5–0.9 pc. The strongest emission of both lobes occurs towards the center of the complex. In the region between the two bubbles, the continuum emission seems to be strongly reduced. At the same time, as seen in Fig. 13, dust continuum emission at 870 μm appears to lie in between the two bubbles. This constellation resembles the famous bipolar H II region S106 (e.g., Bally et al. 1983), and it is likely that both lobes share a common origin within the dust ridge separating the two lobes. In contrast to S106, no ionizing source is detected in the 5.8 GHz data between the lobes.

thumbnail Fig. 12.

Continuum image of the H II region G28.594−0.359 from the combined VLA D+B-configuration data (left), and an MIPSGAL 24 μm image with the radio contours overlaid (right). The diffuse emission on both sides are most likely weak residual side lobes.

The lobes blur into two barely resolved emission peaks at 25″ resolution. We detect RRL emission towards both peaks, and fit both spectra assuming Gaussian line profiles. The emission peak is weakly detected at 13 ± 3 mJy beam−1 and 18 ± 3 mJy beam−1 for posistions 1 and 2, respectively. While this corresponds to only 4–6σ, the transition is detected in multiple channels for which we are confident of a detection. As seen in the right panels of Fig. 13, the velocity of the RRL emission roughly agrees with the peak velocities of the 13CO (1–0) emission across the region, implying that molecular and ionized gas are kinematically connected. We note that small differences exist. Towards positions 1 and 2, the RRL velocities appear slightly blueshifted from the main peak of the CO emission, which is even more clearly seen at higher angular resolution in the 13CO (3–2) transition obtained from the CHIMPS survey (Rigby et al. 2016). This may be indicative of expansion of gas away from the host molecular cloud.

thumbnail Fig. 13.

Overview of the RRL emission of the H II region G28.59−0.364. The left panel shows integrated, stacked RRL emission at 25″ resolution. The GLOSTAR broadband 5.8 GHz continuum (gray contours) from −0.005 Jy beam−1 in steps of 0.01 Jy beam−1. ATLASGAL 870 μm emission (Schuller et al. 2009) is shown (black contours) starting from 0.2 Jy beam−1 in steps of 0.2 Jy beam−1. The right panel shows 13CO (3–2) emission (in red) from the CHIMPS survey (Rigby et al. 2016). All data have been smoothed to the angular resolution of the RRL data of 25″. The positions of extracted spectra in the side panels are indicated with blue crosses.

Morphological, the location of ionized and molecular gas may indicate a physical connection between them. As an indicator for the morphology of the dense molecular gas we use the 870 μm dust emission (Fig. 13, black contours) from ATLASGAL (Schuller et al. 2009) as well as the integrated 13CO (3-2) emission between 86 km s−1 and 96 km s−1 (Rigby et al. 2016). Three ATLASGAL clumps (Contreras et al. 2013; Urquhart et al. 2014) are located in the region. The source closest to the position of the continuum emission, AGAL028.596−00.361, overlaps with the position of the gap between the two radio lobes, and peaks slightly offset towards higher Galactic latitudes. The other two sources are located below the radio lobe at low Galactic latitudes, AGAL028.601−00.377, and above the radio lobe at higher Galactic latitudes, AGAL028.579−00.341. All three ATLASGAL sources are classified as young stellar objects in Urquhart et al. (2018), and have similar masses of log M/M = 2.9 and luminosities of log L/L  =  4.4, 4.1, and 3.8, respectively. The sources appear to be morphologically connected to the radio lobes, as the 5 cm continuum emission extends towards both sources and also slightly brightens towards them (Fig. 13; the same holds for the emission at 24 μm). We speculate that the H II regions have either cleared out the gaps seen in the 870 μm emission in an originally elongated molecular cloud during their expansion, or that the radio lobes simply expanded into spaces of less dense molecular gas, possibly originating from fragmentation of the parent molecular cloud into three denser clumps.

6.4.2. G29.93−0.03

We chose the H II region and molecular cloud complex G29.93−0.03, also known as W43-south, as a demonstration region for the collective use of the different observed tracers in the GLOSTAR survey. W43-south is a site of active star formation (e.g., Reifenstein et al. 1970; Smith et al. 1978). Together with the high-mass star-forming complex W43-main it constitutes the W43 star-forming complex. Both clouds are potentially physically connected (Nguyen Luong et al. 2011). The entire complex is located at an average distance of 5.5 kpc (Zhang et al. 2014) in the Scutum-Centaurus arm and at the end of the Galactic bar (Nguyen Luong et al. 2011; Carlhoff et al. 2013). Their interaction may give rise to the complex dynamics of the region (e.g., Nguyen Luong et al. 2011; Beuther et al. 2017). Since the properties of the ionized gas in this region are well known (e.g., Beltrán et al. 2013), W43-south is well-suited to demonstrate the survey data.

With GLOSTAR, we observe tracers of different stages of the star formation process, and at the same time we observe these at different scales. With Effelsberg we provide important short-spacing information for the interferometry maps. In terms of spatial scales, the Effelsberg observations trace extended continuum radiation at C band from thermal and non-thermal emission at a spatial resolution of 3–4 pc at the distance of W43-south, while the VLA observations allow us to map the H II region complex at a resolution of ∼0.5 pc (D-configuration data) and to distinguish individual (ultra-)compact H II regions at scales of ∼0.05 pc or ∼10 000 AU (B-configuration data). Similar considerations hold for H2CO and the RRLs, for which the observations give information on the extended and on the small-scale structures.

W43-south hosts many H II regions, powered by multiple O and B stars (e.g., Beltrán et al. 2013). Figure 14 shows a three-color composite image of Spitzer IRAC 8 μm, MIPSGAL 24 μm, and GLOSTAR VLA D+Effelsberg 5.8 GHz emission. The region harbors multiple H II regions. Some of them have formed cavities in the surrounding molecular cloud, which are signs of already more advanced stages of star formation. They are filled with 24 μm emission, tracing hot dust, and 5.8 GHz emission from free-free emission. The cavities are confined by photon dominated regions (PDRs) that can be most clearly seen in the high-resolution 8 μm data, tracing polycyclic aromatic hydrocarbon (PAH) emission.

thumbnail Fig. 14.

Multi-color image of GLIMPSE 8 μm (green, Churchwell et al. 2009), MIPSGAL 24 μm (red, Carey et al. 2009), and GLOSTAR VLA D+Effelsberg 5.8 GHz emission (blue) of the G29.93−0.03 (W43-south) star formation complex. Square-root scaling was used and the individual data sets were truncated at 500 and 1000 MJy sr−1 for the 8 and 24 μm data, respectively, and at 20 mJy beam−1 for the centimeter emission. Saturated pixels in the MIPSGAL maps were replaced with the truncation value. The data are shown in their native resolution. For reference, the markers from Fig. 15 are overplotted. The GLOSTAR 5.8 GHz data are repeated as contours for clarity, in steps of 15, 20, 30, 45, 100, 200, 300, and 500 mJy beam−1.

The well-studied hot core G29.96−0.02 is an example of high-mass star formation in an early stage (e.g., Cesaroni et al. 1994, 1998; Gibb et al. 2004). In close proximity is a well-known cometary H II region (e.g., Wood & Churchwell 1989), which can be seen in the GLOSTAR B-configuration data in Fig. 15. Starting from the inlay on the right, the image shows the positions of different methanol maser emission peaks determined from the GLOSTAR B configuration towards the hot core G29.96−0.02 (e.g., Walsh et al. 1998; Minier et al. 2001). We fitted the positions of the peaks at different velocities with 2D Gaussians and find the velocity to be decreasing with distance to the UCH II region. While the precise overall location of the masers with respect to the dense molecular gas may slightly be affected by systematic uncertainties (see Sect. 4.1.4), the direction of the velocity gradient roughly follows the known gradients seen in molecular gas tracers (e.g., Olmi et al. 2003; Beuther et al. 2007; Beltrán et al. 2011). It also appears to be misaligned with the direction of the known molecular outflow of the source (Gibb et al. 2004).

thumbnail Fig. 15.

Overview of the RRL emission in the star-forming complex around l = 29.93°, b = −0.03°. The central panel shows integrated emission between 40 and 140 km s−1 after stacking seven RRLs in velocity at 25″ resolution. The GLOSTAR 5.8 GHz D-array continuum is shown (gray contours) always increasing by a factor of two starting from 10 mJy beam−1. ATLASGAL 870 μm emission (Schuller et al. 2009) is shown (black contours) increasing by a factor of two starting from 0.5 Jy beam−1. The positions of extracted spectra in the side panels are indicated with blue crosses; detected CH3OH 6.8 GHz masers are indicated by cyan crosses. The side panels on the left compare the RRL spectra to 13CO (3–2) emission from the CHIMPS survey (Rigby et al. 2016), and to the H2CO absorption at 0.5 km s−1 spectral resolution from GLOSTAR. All data have been smoothed to 25″ resolution. The right panel shows a zoom-in on the cometary H II region G29.96−0.02 in 5.8 GHz continuum emission from the GLOSTAR survey in B configuration at 2″ resolution. Overlaid with cyan crosses are fitted CH3OH maser position peaks at different velocity channels from GLOSTAR (1.4″ × 1.0″). SMA 862 μm emission from Beuther et al. (2007) is shown (black contours) at 83, 105, 147, and 168 mJy beam−1.

Turning to the entire H II region complex, the middle panel of Fig. 15 shows the integrated RRL emission across the region and methanol masers recovered in the GLOSTAR data. Further spectral lines from the GLOSTAR survey can be seen in spectra shown in the left panels of Fig. 15. The spectra are shown towards position 1, the cometary H II region at G29.96−0.02 and towards position 2 which is a bright H II region, whose ionized gas radiation is equivalent to be powered by a star of spectral type O5, the most powerful star in the region (Beltrán et al. 2013). We map the widely studied formaldehyde transition at 4.8 GHz (blue; e.g., Wilson 1972) and find it to be well-matched to other molecular gas tracers, such as the 13CO (3-2) emission shown here. The stacked RRL emission spectra shown in red are two examples of the widespread RRL emission seen in the middle panel of Fig. 15, which provide kinematic information on the ionized gas. This brief overview of W43-south hence illustrates the quality of the data and possibilities for future study.

7. Conclusion

We presented an overview of a new radio continuum and spectral line survey of 145 square degrees of the northern Galactic plane obtained with the VLA and the 100-m Effelsberg telescopes in the frequency range of 4–8 GHz. After a detailed description of the observational setup, and the calibration and imaging techniques we presented a few selected scientific results that show the quality of the survey data and allows a glimpse of the broad range of scientific topics that can be addressed by the GLOSTAR survey. These will be investigated in more detail in several upcoming publications that are already in preparation.


1

Data from this and various other large-scale centimeter-wavelength surveys can be accessed via the MPIfR Survey Sampler at https://www.mpifr-bonn.mpg.de/survey.html

3

Initially known as the Expanded VLA (EVLA).

4

See http://bessel.vlbi-astrometry.org for more details.

9

The 100-m telescope at Effelsberg is operated by the Max-Planck-Institut für Radioastronomie (MPIFR) on behalf of the Max-Planck Gesellschaft (MPG).

Acknowledgments

We thank the anonymous referee for providing useful suggestions and comments, which helped to improve the manuscript. This research made use of Astropy (http://www.astropy.org), a community-developed core Python package for Astronomy (Astropy Collaboration 2013, 2018), and related packages such as Spectral-Cube and Reproject, as well as of APLpy (Robitaille & Bressert 2012), an open-source plotting package for Python. Early work on the project described here was supported by the European Research Council (ERC) via the ERC Advanced Investigator Grant 247078 (GLOSTAR: A Global View of Star Formation in the Milky Way) awarded to K.M.M, and a Marie Curie International Outgoing Fellowship (No. 275596) awarded to A.B., while H.B. acknowledges support from the Horizon 2020 Framework Programme via the ERC Consolidator Grant CSF-648505. H.B. also acknowledges support from the Deutsche Forschungsgemeinschaft in the Collaborative Research Center (SFB 881) “The Milky Way System” (subproject B1). N.R. acknowledges support from MPG through Max-Planck India partner group grant.

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All Tables

Table 1.

Observed lines, bandwidth, number of channels and polarization products, channel spacings, velocity coverage, and theoretical sensitivity for two visits of one pointing (for the full 1 GHz for the continuum and 1 channel for spectral lines) of the VLA observations.

Table 2.

Selection of spectral lines covered with the GLOSTAR Effelsberg observations.

All Figures

thumbnail Fig. 1.

Pointing configuration of a single observation spanning the range of 35° < l < 36° and |b|< 1°. The background image shows our D-configuration continuum data. Also shown are the primary beam sizes at the center frequency of the higher frequency continuum band (6.9 GHz) of one central pointing and its six neighboring pointings.

In the text
thumbnail Fig. 2.

uv-coverage of a single source at high declination from the D configuration (left) and B configuration (right) observations. While both configurations probe very different ranges, there is significant overlap in the center that allows the combination into a single image. Part of this overlap is due to the large bandwidth covered by the observations.

In the text
thumbnail Fig. 3.

Zero-level shift correction for the Effelsberg data. (a) Effelsberg 4.8 GHz continuum image. (b) Urumqi 6 cm continuum emission overlaid with the Effelsberg 4.8 GHz continuum contours. Both data sets have been convolved to an angular resolution of 15′. The contours start at 50 mK, and each contour is twice the previous one. (c) Difference map derived by subtracting the Urumqi 6 cm continuum emission from the Effelsberg 4.8 GHz continuum map in Fig. 3b. (d) Extended emission component of Fig. 3c derived by the background filter method. (e) Compact emission component derived by the background filter method. (f) Restored Effelsberg 4.8 GHz continuum image.

In the text
thumbnail Fig. 4.

Comparison of peak fluxes of several sources for the Effelsberg and VLA images. The solid line denotes a 1:1 ratio.

In the text
thumbnail Fig. 5.

Radio continuum image of the pilot region in the range 28° < l < 36°. Top: combination of the VLA D configuration and the Effelsberg single-dish images. Bottom: D configuration VLA image of the full continuum of the same longitude range already shown in Medina et al. (2019).

In the text
thumbnail Fig. 6.

Comparison of a smaller region between the D configuration and Effelsberg combination (left), the D configuration only (middle left), the combination of D and B configurations (middle right), and the B configuration only (right).

In the text
thumbnail Fig. 7.

Continuum images of the supernova remnant G28.78−0.44 from the VLA D-configuration data in total intensity (left) and polarized intensity with electric field vectors (right).

In the text
thumbnail Fig. 8.

From left to right: images from D, D+B, and B configurations of G28.2−0.04.

In the text
thumbnail Fig. 9.

Peak intensity maps (PIM) over the velocity range of the methanol maser source G35.197−0.743 and spectra obtained from VLA data. On the left is the VLA D configuration data, which has an average beamsize of ∼18 arcsec. When observed in the B configuration (with beamsize ∼1.5 arcsec, middle panel), one can see that the higher resolution allows us to resolve the maser into two sources. Viewing the spectra on the right, we see that the first peak at 28.51 km s−1 belongs only to the southern source while the rest belong to the northern source. The white contours mark the GLOSTAR radio continuum emission.

In the text
thumbnail Fig. 10.

Methanol maser spectra of source G30.851+0.122. Shown are the GLOSTAR spectra in black and red solid lines for D configuration and B configuration, respectively. The dashed blue line is the MMB spectrum of the corresponding source. The right inset depicts a zoom-in of the velocity component, which shows a difference in intensity between the two configurations; it is spatially unresolved in D and in B configuration.

In the text
thumbnail Fig. 11.

Formaldehyde maser in G32.744−0.076. Top: peak intensity map of known 4.8 GHz formaldehyde maser G32.744−0.076 (Araya et al. 2015) using GLOSTAR VLA D-configuration data and the continuum emission (white contours). Bottom: spectra extracted from GLOSTAR (solid black line) and from the Araya et al. (2015) paper (dashed red line). Despite the lower sensitivity of our data, the faint superimposed absorption feature can be seen.

In the text
thumbnail Fig. 12.

Continuum image of the H II region G28.594−0.359 from the combined VLA D+B-configuration data (left), and an MIPSGAL 24 μm image with the radio contours overlaid (right). The diffuse emission on both sides are most likely weak residual side lobes.

In the text
thumbnail Fig. 13.

Overview of the RRL emission of the H II region G28.59−0.364. The left panel shows integrated, stacked RRL emission at 25″ resolution. The GLOSTAR broadband 5.8 GHz continuum (gray contours) from −0.005 Jy beam−1 in steps of 0.01 Jy beam−1. ATLASGAL 870 μm emission (Schuller et al. 2009) is shown (black contours) starting from 0.2 Jy beam−1 in steps of 0.2 Jy beam−1. The right panel shows 13CO (3–2) emission (in red) from the CHIMPS survey (Rigby et al. 2016). All data have been smoothed to the angular resolution of the RRL data of 25″. The positions of extracted spectra in the side panels are indicated with blue crosses.

In the text
thumbnail Fig. 14.

Multi-color image of GLIMPSE 8 μm (green, Churchwell et al. 2009), MIPSGAL 24 μm (red, Carey et al. 2009), and GLOSTAR VLA D+Effelsberg 5.8 GHz emission (blue) of the G29.93−0.03 (W43-south) star formation complex. Square-root scaling was used and the individual data sets were truncated at 500 and 1000 MJy sr−1 for the 8 and 24 μm data, respectively, and at 20 mJy beam−1 for the centimeter emission. Saturated pixels in the MIPSGAL maps were replaced with the truncation value. The data are shown in their native resolution. For reference, the markers from Fig. 15 are overplotted. The GLOSTAR 5.8 GHz data are repeated as contours for clarity, in steps of 15, 20, 30, 45, 100, 200, 300, and 500 mJy beam−1.

In the text
thumbnail Fig. 15.

Overview of the RRL emission in the star-forming complex around l = 29.93°, b = −0.03°. The central panel shows integrated emission between 40 and 140 km s−1 after stacking seven RRLs in velocity at 25″ resolution. The GLOSTAR 5.8 GHz D-array continuum is shown (gray contours) always increasing by a factor of two starting from 10 mJy beam−1. ATLASGAL 870 μm emission (Schuller et al. 2009) is shown (black contours) increasing by a factor of two starting from 0.5 Jy beam−1. The positions of extracted spectra in the side panels are indicated with blue crosses; detected CH3OH 6.8 GHz masers are indicated by cyan crosses. The side panels on the left compare the RRL spectra to 13CO (3–2) emission from the CHIMPS survey (Rigby et al. 2016), and to the H2CO absorption at 0.5 km s−1 spectral resolution from GLOSTAR. All data have been smoothed to 25″ resolution. The right panel shows a zoom-in on the cometary H II region G29.96−0.02 in 5.8 GHz continuum emission from the GLOSTAR survey in B configuration at 2″ resolution. Overlaid with cyan crosses are fitted CH3OH maser position peaks at different velocity channels from GLOSTAR (1.4″ × 1.0″). SMA 862 μm emission from Beuther et al. (2007) is shown (black contours) at 83, 105, 147, and 168 mJy beam−1.

In the text

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