Free Access
Issue
A&A
Volume 586, February 2016
Article Number A5
Number of page(s) 12
Section Stellar structure and evolution
DOI https://doi.org/10.1051/0004-6361/201527128
Published online 19 January 2016

© ESO, 2016

1. Introduction

The chemical evolution of evolved stars between 0.8–10 M on the asymptotic giant branch (AGB) is driven by thermal pulses (TP). Thermal runaway burning of helium in a shell around the dormant carbon–oxygen core leads to a mixing of the inner layers of the star, resulting in an intricate nucleosynthetic network and the production of new heavy elements (e.g. Karakas & Lattanzio 2007). These elements are mixed to the surface of the star through deep convection during the third dredge-up after the pulse and are incorporated into the stellar wind. The winds from AGB stars replenish the interstellar medium (ISM) with this newly processed material (e.g. Schneider et al. 2014). The stellar mass loss is high enough (up to 10-4 M yr-1) to eventually terminate the evolution of the star on the AGB with most of the stellar mass lost to the ISM (e.g. Herwig 2005). As such, AGB stars are significant contributors to the chemical evolution of the ISM and galaxies. The material is included in molecular clouds where new stars and planets are formed.

The phase of rapid helium burning during a TP cycle lasts only a few hundred years (Vassiliadis & Wood 1993). Although the helium luminosity experiences a large increase, the surface luminosity only increases slightly. However, this increase in luminosity leads to additional radiation pressure on the dust grains in the upper atmosphere of the star and, combined with a lower temperature and larger radius, results in an increased mass-loss rate and expansion velocity. After He-burning ceases, the surface luminosity, and hence the mass-loss rate and expansion velocity, decrease again (Steffen & Schönberner 2000; Mattsson et al. 2007).

An indication of highly variable mass loss from AGB stars was first observed in CO emission in the form of detached shells around carbon AGB stars, and a formation connected to TPs was suggested (Olofsson et al. 1988, 1990). Since then, detached shells of dust and gas around ~ten carbon AGB stars have been observed. The strongest argument for the connection between detached-shell sources and TPs are the detection statistics that are based on a volume-limited sample of carbon stars (Olofsson et al. 1993). No detached CO shells have been observed around oxygen-rich (M-type) AGB stars, where dust opacity effects possibly prevent the formation of a shell during the TP (e.g. Bladh et al. 2015). The formation mechanism is also fundamentally different from the shells observed around high-mass evolved stars, where photoionization creates confined shells (Mackey et al. 2014). Thermal emission from the dust in detached shells was first observed in the far-infrared by IRAS (van der Veen & Habing 1988; Waters et al. 1994; Izumiura et al. 1997), and more recently by AKARI and Herschel (Kerschbaum et al. 2010; Izumiura et al. 2011; Cox et al. 2012; Mečina et al. 2014). Most of these shells are likely connected to TPs. The images make it possible to determine the dust temperature in the detached shells and, to some extent, the sizes of the shell. Observations of dust scattered, stellar light in the optical have given a detailed view of the dust distribution in the shells, most recently in scattered polarised light of the detached shell sources R Scl and V644 Sco (González Delgado et al. 2001, 2003; Olofsson et al. 2010; Maercker et al. 2010, 2014; Ramstedt et al. 2011). In comparison to single-dish (SD) observations of CO line emission and images of dust in the far infrared, the optical observations of dust scattered light provide information at high angular resolution. Observations at high-angular resolution of the detached gas shells in CO emission have only been done for the detached shell sources TT Cyg (Olofsson et al. 2000) and U Cam (Lindqvist et al. 1999) using the Plateau de Bure Interferometer, and R Scl (Maercker et al. 2012) using the Atacama Large Millimeter/submillimeter Array (ALMA). The observations clearly show the detached shells around TT Cyg and U Cam at 35′′ and 7.̋3, respectively. No emission is detected between the shells and the present-day mass-loss, implying that the mass-loss rate decreased significantly after the TP, leading to the formation of an expanding shell that is not connected to the present-day mass-loss (and hence detached). The recent observations with ALMA during Cycle 0 imaged the detached shell around R Scl in 12CO(3−2) emission at high angular resolution (1.̋4 beam; Maercker et al. 2012), showing a clumpy structure and slight deviations from spherical symmetry in the shell. In addition to the detached shell, the data also show a spiral structure that connects the shell with the present-day mass-loss. The spiral is formed by the interaction of the stellar wind with a previously unknown binary companion, and allows us to determine the evolution of the mass-loss rate and expansion velocity since the last TP. These are the first observational constraints of the behaviour of the stellar mass loss during and after a TP. While the evolution generally fits with theoretical predictions, it is clear that the mass-loss rate must decrease significantly slower than predicted by models. These observations already show that the shell around R Scl is not entirely detached. Comparing the distribution of the gas shell with images of polarised, dust scattered stellar light showsthat the dust and gas have an almost identical distribution in the shell, implying a common evolution of the dust and gas shells since the last TP (Maercker et al. 2014).

Maercker et al. (2012) only discuss the ALMA observations of 12CO(3−2) observed towards R Scl, and focus on the hydrodynamical modelling of the spiral structure. We here present the full set of 12CO observations of the circumstellar environment around R Scl, concentrating on the overall CO emission. In Sect. 2 we present the ALMA observations of 12CO(1−0), 12CO(2−1), and 12CO(3−2). We also present new SD observations of 12CO(2−1) and 12CO(3−2) taken with the Atacama Pathfinder Experiment telescope (APEX). In Sect. 3 we describe our analysis strategy and the results, and in Sect. 4 we discuss what this implies for the physical properties of the gas shell and its origin. Our conclusions are finally presented in Sect. 5.

In previous publications, the shells of gas found around carbon AGB stars are referred to as detached shells. At least in the case of R Scl there are clear signs that the shell is in fact not detached; Sects. 2.4 and 3.3. Throughout the paper we will therefore refer to the shell around R Scl, meaning the thin shell of dust and gas found at 19.̋5 from the star. We will refer to the gas between the shell and the star as the circumstellar envelope (CSE).

Table 1

Summary of the reduced image cubes of the ALMA observations of the circumstellar environment of R Scl.

thumbnail Fig. 1

ALMA observations of 12CO(1−0) towards R Scl. The bin size of each panel is 1.5 km s-1. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner.

2. Observations

2.1. R Sculptoris

thumbnail Fig. 2

ALMA observations of 12CO(2−1) towards R Scl. The bin size of each panel is 1.0 km s-1. Panels with a spacing of 2 km s-1 are shown. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner.

thumbnail Fig. 3

ALMA observations of 12CO(3−2) towards R Scl. The bin size of each panel is 0.5 km s-1. Panels with a spacing of 1.5 km s-1 are shown. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner. These data were first presented in Maercker et al. (2012).

R Scl is a semi-regular pulsating carbon AGB star with a pulsation period of approximately 370 days. Current distance estimates are very uncertain, ranging from 266 pc (revised Hipparcos, Knapp et al. 2003) to 370 pc (using K-band Period-Luminosity relationships; Knapp et al. 2003; Whitelock et al. 2008). Integrating the spectral energy distribution of R Scl and assuming a distance of 370 pc gives a luminosity of L = 5200 L – a reasonable value for carbon AGB stars. We will use 370 pc throughout this paper, noting the high uncertainty in this value. Maercker et al. (2012) use a distance of 290 pc, adopting a value that was erroneously calculated from a period-luminosity relationship in Schöier et al. (2005). This does not affect the main conclusions in Maercker et al. (2012), but changes the estimated age of the shell around R Scl from 1800 yr to 2300 yr. The estimated mass-loss rates also slightly increase.

The stellar velocity is determined from molecular line observations to be νLSR=19\hbox{$\varv_{\rm{LSR}}^*=-19$} km s-1. R Scl is surrounded by a thin shell of dust and gas. The radius and width of the shell were measured with high precision in images of dust scattered, stellar light, to be 19.̋5 ± 0.̋5 and 2′′± 1′′ (Olofsson et al. 2010; Maercker et al. 2014), respectively, and the dust-shell radius and width were found to coincide nearly exactly with the shell of gas observed in 12CO(3−2) with ALMA (Maercker et al. 2014).

2.2. ALMA early science observations

R Scl was observed during ALMA Cycle 0 using the compact configuration of the main array. The main target of the observations were the 12CO(1−0) line in Band 3, the 12CO(2−1) line in Band 6, and the 12CO(3−2) line in Band 7. The parameters of the final reduced images are given in Table 1. Channel maps of the three 12CO transitions are shown in Figs. 1 to 3. The observational setup is summarised in Table 2 and described below. In Cycle 0 ALMA did not offer the Atacama compact array (ACA) yet, and the data are hence limited by the largest observable scales in the respective transitions. The spectral setup in Cycle 0 allowed us to define (with some restrictions) four spectral windows (spw) with the same bandwidth (BW) and channel width. In all bands pointed mosaics were observed to cover the entire area of the detached shell. The observations are divided into individual scheduling blocks (SBs). The delivered data was re-reduced to improve the data quality using version 4.1 of the Common Astronomy Software Application (CASA), making use of python scripts to automate the calibration process. The SBs are calibrated separately and then combined for the respective bands. After calibration, imaging of the CO emission lines was carried out with the CLEAN algorithm using natural weighting and binning the spectra. The complex structures of the CO envelope were masked in an iterative procedure with decreasing thresholds in CLEAN. Band 3: observations of the 12CO(1−0) emission line at 115.27 GHz were carried out between Jan. 23 and Jan. 25 2012. The dataset contains two SBs, taken in the two consecutive nights. Unfortunately, water vapour radiometer (WVR) measurements with sufficient quality were only available for one of the SBs, meaning that rapid atmospheric variations were only corrected for half of the data. One SB revealed very low quality data of the flux calibrator Callisto. Therefore the flux densities of the calibrators were adopted from the other SB. However, the entire spectral window containing the CN(N = 1–0) emission had to be excluded from further investigation because of a very low signal-to-noise ratio, making the data unusable.

Band 6: observations of the 12CO(2−1) emission line at 230.54 GHz were carried out on Oct. 1 2011. The dataset contains two SBs.

Band 7: observations of the 12CO(3−2) emission line at 345.80 GHz were carried out between Oct. 3 and Oct. 19 2011. The dataset contains a total of seven SBs. One SB did not contain flux calibrator measurements, forcing us to use the flux calibration data from the other SBs.

Table 2

Summary of ALMA observations of the circumstellar environment of R Scl.

2.3. Single-dish observations

In order to estimate the amount of extended emission that goes beyond the largest recoverable scales in the ALMA observations, we compare the ALMA spectra to SD spectra. For the 12CO(1−0) transition we use spectra from the Swedish-ESO submillimeter telescope (SEST, with a beam full width half maximum (FWHM) of 44′′; Olofsson et al. 1996) and the IRAM 30 m telescope (with a beam FWHM of 22′′; Olofsson et al. 1993).

For the 12CO(2−1) and 12CO(3−2) transitions we observed two on-the-fly (OTF) maps with APEX. The observations were done using the APEX-1 and APEX-2 receivers for 12CO(2−1) and 12CO(3−2), respectively (Vassilev et al. 2008). The beam FWHM is 27′′ in the 12CO(2−1) transition and 18′′ in the 12CO(3−2) transition. The maps are sampled at 1/3 of the beam-widths and cover areas of 45′′× 45′′ and 54′′× 54′′, respectively. The total on-source integration of respectively 12.5 min and 13.5 min resulted in rms values of 0.07 K and 0.18 K. Figure 4 shows the SD observations. Spectra were extracted from the pixel in the APEX OTF maps centred on the star, giving a spectrum equivalent to a single pointing on the star with the beam of APEX at the respective frequency. The observations are summarised in Table 3.

2.4. Interferometer vs. single-dish observations and extended emission

Figure 4 shows a comparison of observed SD spectra with the equivalent ALMA spectra extracted from maps that were smoothed to the same respective beams using the task imsmooth in CASA. Depending on the frequency and array configuration, the interferometer will resolve out flux coming from spatial scales that are larger than the largest recoverable scale (Table 2), leading to negative features in the images. The comparison to the SD spectra shows that the ALMA observations miss flux in all the observed emission lines:

The front and back of the shell: One would expect the least amount of flux to be lost at the extreme velocities, where the emission only comes from the front and back caps of the shell and is comparatively compact, while the emission may be more extended at the νLSR\hbox{$\varv_{\rm{LSR}}^*$} due to an extended envelope (see below). For 12CO(1−0) we see that this is indeed the case, where we recover all emission at projected velocities |νLSRνLSR|>11\hbox{$|\varv_{\rm{LSR}}-\varv_{\rm{LSR}}^*|>11$}, while we only recover about 60–70% of the flux at the νLSR\hbox{$\varv_{\rm{LSR}}^*$}. For the 12CO(2−1) transition the observations recover 70% of the flux at the extreme velocities, while only 35% is recovered at the νLSR\hbox{$\varv_{\rm{LSR}}^*$}. Finally, 60–70% of the flux is recovered at all velocities for the 12CO(3−2) line1.

At the extreme velocities the geometry of the shell (expansion velocity, shell thickness, and turbulent velocity) causes the caps to have an apparent size that can be larger than the largest recoverable scales. For a shell radius of Rsh = 19.̋5, a shell width of ΔRsh = 2′′ (Maercker et al. 2014), and an expansion velocity of νsh = 14.3 km s-1, the size of the cap at the extreme velocity would be 18′′ at 1.5 km s-1 resolution in 12CO(1−0), 15′′ at 1 km s-1 resolution in 12CO(2−1), and 11′′ at 0.5 km s-1 resolution in 12CO(3−2). For 12CO(2−1) and 12CO(3−2) this is indeed larger than the maximum recoverable scale, explaining the lost flux.

The CSE and shell: The amount of flux lost in the different transitions at the νLSR\hbox{$\varv_{\rm{LSR}}^*$} constrains the extended emission of the CSE. In the 12CO(1−0) emission (Fig. 1) the shell can barely be discerned and the spiral shape observed in 12CO(3−2) (Maercker et al. 2012) disappears almost entirely. Instead the ALMA observations show a bowl-like shape with no emission at the stellar position. This can be explained with a shell that is entirely filled with 12CO(1−0) emission, with a low contrast between the extended emission and the small-scale structure (i.e. the shell and spiral). While the SD observations detect all the extended emission inside the shell, the ALMA observations resolve-out the flux at large scales, leading to the observed bowl-like shape. In the 12CO(2−1) emission (Fig. 2) the shell is more pronounced and the spiral shape can be seen. However, the structure still lies on top of an overall bowl-like shape, with the present-day mass loss only barely detected. Such an observed intensity distribution can be explained by slightly less extended 12CO(2−1) emission, and a higher contrast between the small-scale structures and the extended emission (i.e. less flux gets resolved out compared to the 12CO(1−0) emission, and the small-scale structures are more pronounced). In the 12CO(3−2) emission (Fig. 3) the shell, spiral, and present-day mass loss are clearly visible, and the lost flux is apparent in the form of negative features around the observed structure. This implies a relatively limited extent of the 12CO(3−2) emission that is centrally peaked. The maximum recoverable scales for the different transitions in Table 2 give an indication of the minimum size of the emitting regions for the individual lines, while the beam FWHMs of the SD spectra give a rough upper limit (depending on whether the line profiles are spatially resolved or unresolved). This confirms that the 12CO(1−0) emission must extend almost out to the shell, causing the smooth distribution and lack of central emission observed in the ALMA data, while the 12CO(2−1) emitting region is limited to radii up to 13′′–15′′, and the 12CO(3−2) emission comes from a radius up to 10′′. Extended emission from 12CO reaching out to the shell means that the shell is in fact not detached, but instead filled with significant amounts of molecular gas.

Table 3

Summary of single-dish (SD) observations towards R Scl.

thumbnail Fig. 4

SD observations towards R Scl (from left to right): SEST CO(1–0), IRAM 30 m CO(1–0), APEX CO(2–1), and APEX CO(3–2). The FWHM of the SD beams are 44′′, 22′′, 27′′, and 18′′, respectively. The red spectra show the ALMA observations of the respective transitions convolved with Gaussian beams to give the FWHM from the respective telescopes.

In Fig. 5 we use a toy model to simulate extended regions of emission and their effect on the ALMA observations. We create ad-hoc intensity distributions with no underlying physical model to fit the above described scales and reproduce the observed images. The toy-images consist of a clumpy shell with a radius of 19.̋5 and a width of 2′′, a spiral with 4.5 evenly spaced spiral windings, and extended emission in the form of discs with radii of 18′′, 14′′, and 9′′ for the 12CO(1−0), 12CO(2−1), and 12CO(3−2) transitions, respectively, and with a Gaussian drop-off at the edge with σ = 6′′.

Simulations in CASA, using the ALMA Cycle 0 compact configuration in the three bands, show that the observed features can indeed be explained by a shell and spiral shape where the shell is filled with extended emission of varying size (decreasing from 12CO(1−0) to 12CO(3−2)). The toy model qualitatively shows the effects of different intensity distributions, explaining the observations, and serves only as a rough estimate of the spatial scales of the emission. The implications this has for the density distribution within the shell, and hence the evolution of the mass-loss rate during and after the TP, are discussed in Sect. 3.3.

thumbnail Fig. 5

Qualitative analysis of the effect of extended emission on the ALMA Cycle 0 observations of ALMA. The left columns shows toy-models of the emission from the shell around R Scl and extended emission inside the shell at the νLSR\hbox{$\varv_{\rm{LSR}}^*$} for the 12CO(1−0), 12CO(2−1), and 12CO(3−2) transitions (top to bottom, respectively). The right column shows the resulting simulated observations using the ALMA Cycle 0 compact configuration of the main array (simulated using the CASA simulator).

3. Analysis and results

We extract the shell emission from the ALMA observations, allowing us to analyse the shell and CSE separately. Our analysis and results focus on the properties of the shell and on the information we can gain about the distribution of the molecular gas of the CSE to constrain the recent mass-loss evolution. We do not treat the spiral. A detailed analysis of the spiral shape observed in 12CO(3−2) was done using hydrodynamical models (Maercker et al. 2012). Any additional detailed analysis of the CSE structure would require high spatial-resolution observations of the spiral shape to constrain essential parameters such as the binary separation, the shape of the inner spiral, and the contrast between the spiral and inter-spiral material. Such observations are in progress during the current ALMA Cycle (Cycle 2).

3.1. The shell morphology

The shell morphology is best described based on the 12CO(3−2) images, where the ALMA observations give the highest spatial resolution. Overall the shell has a spherical appearance in all velocity channels. Fitting a spherically symmetric shell with a radius of 18.̋5 expanding at 14.3 km s-1 reproduces the observed size of the shell in all channels (Maercker et al. 2012). Limb brightening along the inner edge of the shell slightly moves the peak inwards (Maercker et al. 2010; Olofsson et al. 2010), and the radius measured in the ALMA data is consistent with the 19.̋5 measured in polarised, dust-scattered light of the shell around R Scl (Maercker et al. 2014).

However, clear deviations from a perfect sphere are apparent. This was already observed in the dust observations (Maercker et al. 2014), which show an almost identical distribution to the 12CO(3−2) from ALMA. In particular there is a flattening of the southern part of the shell at the νLSR\hbox{$\varv_{\rm{LSR}}^*$}. The shell also appears strongly disrupted in this region. The same structures can also be seen in the 12CO(2−1) maps, and to some degree in the 12CO(1−0) maps, where the lower angular resolution, however, smoothes most features out.

thumbnail Fig. 6

ALMA 12CO observations of the shell for 12CO(1−0), 12CO(2−1), and 12CO(3−2) (black lines, panels 1–3, respectively). The data are extracted from annuli within ±3′′ from the projected radius of the shell in each velocity bin in the images smoothed to 4′′ resolution. For comparison, the black dotted lines show the emission integrated over the entire image for each velocity bin instead (i.e. also containing emission from the CSE). The red lines show the best-fit model of the shell only. The right panel shows the χ2 map of the radiative transfer models of the shell with shell-mass vs. shell temperature. The colour scale gives the χ2 value, the white cross indicates the best-fit model. The white contours give the 1σ and 2σ levels (the 3σ contours fall outside of the plotted range).

A speculative interpretation of this is an interaction of the binary companion with the stellar wind as the shell is created. The interaction distorts the shell from a spherically symmetric shape, while leaving the shell undisturbed on the opposite side. As the shell expands, the effect of the binary companion is reduced. At the end of the pulse, when the mass-loss rate and expansion velocity start to decline, the spiral formed by the post-pulse mass-loss connects to the shell at position angle PA 90° (with PA = being North, and the PA increasing counter-clockwise). If true, the flattened and disrupted southern part of the shell would indicate the onset of the TP, while the point at which the spiral attaches to the shell marks the end of the TP. The estimated binary period is based on the present-day expansion velocity of the wind and the separation of the inner spiral windings (Maercker et al. 2012) and depends on the estimated distance to the source. Adjusting for the larger distance used here, the binary period is estimated to be 445 yr (Maercker et al. 2012). The fraction of the shell affected by the binary companion would be 40% of one revolution, translating into a TP timescale of 180 yr.

Whether this is a viable scenario has to be tested through detailed hydrodynamical modelling. The morphology of the shell depends on the mass-loss properties, the masses of the stars, and the timescales. ALMA Cycle 2 data will give us the necessary resolution and sensitivity to constrain these critical parameters and to calculate a detailed model of the shell and spiral formation.

3.2. The shell emission

In order to analyse the emission from the shell we extract regions in the channel maps for all three transitions assuming a shell-radius of 19.̋5 and an expansion velocity of 14.3 km s-1 (Maercker et al. 2012, 2014). In order to ensure that the same regions are extracted in each transition, we smoothed the images to a spatial resolution of 4′′ and a velocity resolution of 1.5 km s-1. Although the FWHM of the shell is only 2′′, the spatial and spectral resolution cause a widening of the shell in the images, and the shell emission is extracted from a ring with width ±3′′ centred on the shell. The resulting spectra are shown in Fig. 6 and are compared to the spectra integrated over the entire images.

For a homogeneous spherically symmetric shell one would expect a flat spectrum, i.e. each velocity channel probes the same number of CO molecules in the shell. However, in particular for 12CO(2−1) and 12CO(3−2), it is clear that the shell has a clumpy structure and an asymmetric distribution of CO between the front and the back of the shell. Further, close to the extreme velocities it becomes increasingly difficult to differentiate between shell emission and emission originating from the rest of the CSE. This is particularly true in the case of R Scl where the emission inside the shell has a velocity gradient that gradually decreases from 14.3 km s-1 in the shell to its present-day value of 10.5 km s-1 (Maercker et al. 2012).

In order to determine the mass and temperature in the shell, we calculated a grid of 1-dimensional radiative transfer models based on the monte-carlo technique (Schöier & Olofsson 2001). Each shell has a Gaussian density distribution with a radius of 19.̋5, a FWHM of 2′′, and a constant expansion velocity of 14.3 km s-1. We assume a fractional abundance of 12CO of f(12CO) = 4.3 × 10-4 relative to H2 (Olofsson et al. 1993). This value was derived using the elemental composition given by Lambert et al. (1986). The temperature is assumed to be constant throughout the shell. The grid is calculated for shell-masses between 2.5 × 10-3 M to 4.75 × 10-3M in steps of 0.25 × 10-3 M and temperatures between 10 K to 290 K in steps of 20 K. For each model we determine the best-fit model (Fig. 6) by minimising the χ2 value χ2=(Iobs,iImod,iσobs,i)2,\begin{equation} \label{e:chi2} \chi^2= \left(\frac{I_{{\rm obs},i}-I_{{\rm mod},i}}{\sigma_{{\rm obs},i}}\right)^2, \end{equation}(1)where Iobs,i is the integrated intensity of the observation i, Imod,i is the modelled intensity, σobs,i is the uncertainty in the observation is assumed to be 20%, and the sum goes over all transitions. The best-fit model gives a shell-mass of (4.5 ± 1.5) × 10-3 M at a temperature of 50+200-20\hbox{$^{+200}_{-20}$} K. Note that the radiative transfer model assumes a spherically symmetric, smooth shell, and hence can not reproduce asymmetries within the shell. The observed and modelled line profiles may therefore differ significantly. In the optically thin limit, the integrated intensity still gives a good measure of the total mass and temperature in the shell. The upper limit in the shell mass is only sampled by few points, and hence not included in the χ2 map in Fig. 6. The fractional 12CO abundance further assumes that no 12CO has been photodissociated. Decreasing f(12CO) leads to an increase in the estimated shell mass and a decrease in the shell temperature. For optically thin lines the increase in mass would scale roughly linearly with f(12CO). The lines in our best-fit model have tangential optical depths of τtan ~ 1, meaning that the shell mass clearly would be affected by a change in f(12CO), making the estimated shell mass a lower limit. However, for the mass-loss rate during the creation of the shell (2.3 × 10-5 M yr-1, see below), models of photodissociation predict the half-abundance radius of CO to be significantly larger than the radius of the shell (on the order of 40–50′′; Stanek et al. 1995). A clumpy medium will further protect the 12CO in the shell from dissociation (while still allowing photodissociation in the CSE; see Sect. 3.3), and we do not expect the photodissociation to affect the abundance of 12CO in the shell significantly. We thus consider the estimated mass to be the correct shell mass within the uncertainties.

The estimate of the mass in the gas shell is consistent with previous estimates from Schöier et al. (2005) based on SD data alone (Mshell = 2.5 × 10-3 M). More recently, Olofsson et al. (2015) model the emission of CI from the shell based on SD observations with APEX. Their detection of CI is consistent with the estimated C/O-ratio of R Scl, assuming solar abundances of oxygen, that all neutral carbon comes from the photodissociation of carbon-bearing molecules except for CO, and there is very limited ionisation of C. They determine the physical parameters of the shell using SD spectra of 12CO, including high J-transitions observed with HIFI. Assuming f(12CO) = 10-3, their resulting shell mass is (2 ± 1) × 10-3 M, with a temperature of 100-70+200\hbox{$100^{+200}_{-70}$} K. Hence, using essentially independent methods (interferometry vs. SD observations and an independent consistency check with CI observations), and adjusting for the difference in f(12CO), the same shell masses and temperatures are derived.

The analysis of the 13CO(3−2) emission observed with ALMA suggests that at least parts of the shell must have temperatures that are lower than the derived 50 K (Vlemmings et al. 2013). The measured 12CO/13CO ratio shows regions in which additional 13CO is formed due to chemical fractionation. This process however requires temperatures lower than 35 K. We only model the temperature of a smooth, homogeneous shell, while a clumpy structure will affect the radiative transfer and decouple the connection between mass and temperature.Olofsson et al. (2015) in principle manage to find a satisfying fit for even lower temperatures than 50 K, albeit for unrealistically high shell masses. Shell temperatures of 10 K require masses approaching 1 M. Although this may in principle be possible, the consistency of a shell mass of a few times 10-3 M with various dust estimates (e.g. González Delgado et al. 2003; Schöier et al. 2005; Olofsson et al. 2010) makes a total mass in excess of 0.1 M unlikely (Olofsson et al. 2015).

While the shell is likely confined by collision with a previous, slower wind (e.g. Steffen & Schönberner 2000; Schöier et al. 2005; Mattsson et al. 2007), the mass-loss rate of the previous wind must have been very low (less than a few 10-6 M yr-1). The half-abundance radius due to photodissociation of 12CO lies outside the shell for higher mass-loss rates, but no signs of the spiral structure can be observed outside of the shell. A significant amount of mass outside of the shell would have further led to a deceleration of the shell, which is not observed (Maercker et al. 2012). Hence, we believe that only a minor amount of mass from the previous mass-loss has been swept up in the shell. Assuming a shell-creation time of 200+100-50\hbox{$^{+100}_{-50}$} yr (Vassiliadis & Wood 1993, consistent with the ALMA observations) then leads to a mass-loss rate of (2.3-1.3+1.7)×10-5M\hbox{$(2.3^{+1.7}_{-1.3})\times10^{-5}~M_{\odot}$} yr-1 during the creation of the shell.

3.3. The recent evolution of the stellar wind

In order to constrain the physical parameters of the CSE inside the shell, we convolved the best-fit model of the shell with the SD beams of the respective transitions (Fig. 7, top), and subtract it from the SD observations. The emission from the shell, extracted from the ALMA images, is additionally convolved with the SD beams and compared to the model to ensure that the right flux is subtracted. We find that the clumpy structure is generally smoothed out significantly in the SD observations, giving a good fit of the model to the observations. Using the model instead of the ALMA observations has the advantage that only the shell is subtracted, while the observations may still contain additional velocity components that do not belong to the shell. In difference to the hydrodynamical modelling of the 12CO(3−2) observations (Maercker et al. 2012), we here focus on the overall extended emission from the CSE, instead of the detailed structure.

thumbnail Fig. 7

Top: SD spectra (black, from left to right: SEST 12CO(1−0), IRAM 12CO(1−0), APEX 12CO(2−1), and APEX 12CO(3−2)) with the best-fit shell model convolved with the respective beams (red). The green spectra show the shell emission extracted from the ALMA data and convolved with the respective SD beams. Bottom: SD spectra after subtracting the best-fit shell models. The red lines show the best-fit model fit to the shell-subtracted SD observations to constrain the average mass-loss rate since creation of the shell.

The shell-subtracted SD observations (Fig. 7, bottom) now contain the emission from the CSE without the shell, allowing us to model the mass loss since the creation of the shell. We model the subtracted SD spectra with a single, constant mass-loss rate, while in fact the mass-loss rate likely has varied since formation of the shell. As such we are only modelling an average mass-loss rate inside the shell. A varying mass-loss rate will however affect the density distribution and the emission regions of different CO transitions, making it difficult to find a consistent model for all observed lines. Likewise, the half-abundance radius assumes a constant wind and we are only determining an average radius for the emitting region. Further, the amount of photodissociation inside the shell is not clear as there likely is significant shielding by the shell itself. Finally, the models are very degenerate between the chosen mass-loss rate, half-abundance radius, temperature profile, and velocity profile.

Due to these limitations we only derive a model that fits the subtracted SD spectra assuming reasonable parameters for the temperature and velocity profiles, and loosely constraining the radius of the emitting region by the limits given by the observed scales in the ALMA data (see Sect. 2.4). The derived mass-loss rate serves as an indication of the average mass-loss rate since the formation of the shell.

Assuming a constant mass-loss rate results in a 1/r2 density distribution. The fractional abundance is assumed to follow f(r)=f0exp(ln(2)(rR1/2)a),\begin{eqnarray} \label{e:fcoprofile} f(r)=f_0\,{\rm{exp}}\left(-{\rm{ln}}(2)\left({r \over R_{1/2}}\right)^a\right), \end{eqnarray}(2)where f0 is the initial fractional abundance, R1/2 is the half-abundance radius, and a = 2.5 (Mamon et al. 1988). For the kinetic temperature we assume a power-law of the form Tkin(r) = T0 × (r/R0)β with β = −0.85. R0 is the inner radius of the CSE, assumed to lie at 3 times the stellar radius (assuming a black-body with an effective temperature of 2300 K and luminosity of 5200 L). The velocity increases gradually from 3 km s-1 to 14.3 km s-1 to take into account both the acceleration of the wind in the inner CSE, as well as the time evolution of the terminal wind velocity since creation of the shell.

Using the above assumptions, we manage to model the 12CO(1−0) transition observed with SEST and the 12CO(2−1) transition observed with APEX using a mass-loss rate of 1.6 × 10-5 M yr-1 and a half-abundance radius of 7.̋2. A 12CO radius that is smaller than the shell indicates that the shell is clumpy, and allows for the penetration of photodissosciating radiation into the CSE. The resulting emitting region for 12CO(1−0) is indeed not very centrally peaked and extends out to 18′′, while the 12CO(2−1) emission is more peaked and only extends out to 15′′. The 12CO(3−2) emission is the most compact, extending out to a radius of 11′′. These results are consistent with the limits set by the ALMA and SD data (Sect. 2.4). While the extent of the emitting region in the different transitions is an effect of the excitation conditions, the best-fit model overestimates the emission in the 12CO(1−0) line observed with IRAM and the 12CO(3−2) emission observed with APEX, in particular at the νLSR\hbox{$\varv_{\rm{LSR}}^*$}. For the 12CO(1−0) transition the beam of the IRAM observations probes a much smaller region than the SEST observations (27′′ in diameter vs. 44′′), and hence are dominated by the more recent mass loss from R Scl. The APEX 12CO(3−2) observations also are dominated by the recent mass loss, both due to more centrally peaked 12CO(3−2) emission, as well as due to a smaller beam size (18′′). These two transitions can be modelled with the same half-abundance radius but a mass-loss rate of 3.5 × 10-6 M yr-1, consistent with a continuously declining mass-loss rate since the last TP. The present-day mass-loss rate is estimated to be 3 × 10-7 M yr-1 based on HCN models (Schöier et al. 2005). Additional photodissociation of molecules in the inner wind due to binary interaction (Vlemmings et al. 2013) likely makes this estimate a lower limit, with the true present-day mass-loss rate being closer to 10-6 M yr-1.

Hence, modelling of the shell-subtracted SD data gives a rough picture in which the mass-loss rate decreases gradually by more than an order of magnitude from when the shell was created to today. The mass-loss rate derived by fitting the lines that probe the largest extent of the CSE is only slightly lower than the shell mass-loss rate, implying that the mass loss most likely did not drop very quickly after creation of the shell. In principle it would be possible to attempt to derive a more quantitive evolution of the mass-loss rate since the creation of the shell by modelling a variable mass-loss rate that decreases over time. However, the limits set by the SD spectra are relatively uncertain, and the degeneracies of the model (mass-loss rate, CO photodissociation, temperature profile) are not easily constrained. The loss of extended flux in the current ALMA data prevents using these observations to effectively constrain the mass-loss rate evolution, while the lack of intermediate baselines makes combination with the SD data very uncertain. The ALMA Cycle 2 observations of R Scl will contain Atacama Compact Array (ACA) observations, together with high-resolution main-array observations, and will make a more detailed description of the spiral around R Scl and measure the emission on all spatial scales possible. This together with detailed hydrodynamical modelling will set stronger constraints on the recent mass-loss evolution and the creation of the shell around R Scl.

3.4. An additional velocity component

In the 12CO maps observed with ALMA (Figs. 1 to 3) there is clear emission at velocities ±18 km s-1 relative to the νLSR\hbox{$\varv_{\rm{LSR}}^*$}. The expansion velocity of the shell is 14.3 ± 0.5 km s-1, while the present-day expansion velocity is constrained to less than 10.5 km s-1 by HCN and high-J 12CO line profiles (Schöier et al. 2005; Olofsson et al. 2015). The additional velocity component also becomes evident in the SD spectra after subtracting the shell model (most prominently as a red-shifted peak; Fig. 7). The ALMA maps show that the emission is centred on the star. However, it is not clear what the origin of this higher-velocity component is. The ratio of the high-velocity components between the observed transitions implies that the emission comes from a warm region close to the star. The ratio between the blue and red-shifted parts of this component further indicates emission from an optically thick outflow. A possible explanation would be the onset of a bipolar outflow. If this were an extended outflow, it would have to be exactly along the line of sight, which is unlikely. A compact bipolar outflow would be possible along any direction as long as it does not extend further than the spatial resolution of the 12CO(3−2) map, i.e. 1.̋4. At a distance of 370 pc this corresponds to a physical size of 500 AU in diameter. An alternative explanation may be a recent increase in expansion velocity of a spherical mass-loss. Whether this comes along with an increase in mass-loss rate is uncertain, but it would imply that the evolution of the post-pulse expansion velocity and mass-loss is not necessarily a smooth function of time.

It is not clear which (if any) of the above scenarios can explain the additional emission at higher velocities observed in the 12CO lines. The high spatial-resolution data with ALMA from Cycle 2 will resolve the inner CSE of R Scl with a spatial resolution of 0.̋2. This will help in identifying the origin of the higher-velocity emission.

4. Discussion

For over two decades, the observed, geometrically thin gas shells around a handfull of AGB stars have been connected to TPs. Their formation has been described both theoretically (Steffen et al. 1998; Steffen & Schönberner 2000; Mattsson et al. 2007) and observationally (e.g. Olofsson et al. 1990, 1996, 2010; Schöier et al. 2005; Maercker et al. 2010, 2012, 2014). It is generally assumed that the increase in mass-loss rate and expansion velocity during a TP leads to a higher-mass shell interacting with a low-density, slower pre-pulse wind, confining the shell and preventing it from very quickly dispersing due to internal pressure. After the TP, the mass-loss rate and expansion velocity drop drastically, only slowly recovering to values similar to the pre-pulse mass-loss during the remainder of the TP cycle. The sudden drop in mass-loss rate and expansion velocity leads to the shell detaching entirely from the present-day mass loss, leaving an essentially empty shell. The TP cycle starts with a high mass-loss-rate phase which lasts a few hundred years, followed by an inter-pulse time of several ten thousand years, depending on the mass of the star (Karakas & Lattanzio 2007). In order to form a detached shell, a sufficient change between the pre-pulse and pulse mass-loss rates in combination with a change in expansion velocity is required (Mattsson et al. 2007). The parameters derived in this paper imply a change in mass-loss rate of more than an order of magnitude, accompanied by a change in expansion velocity. The creation of the shell around R Scl is hence consistent with formation during a TP.

However, instead of showing a detached shell without (significant) 12CO emission between the shell and the present-day mass loss, the ALMA observations of the shell around R Scl show a continuous mass-loss rate evolution with a significantly slower decline over time. This leads to a filled shell rather than a detached shell. The derived mass of the shell combined with estimated TP timescales implies a relatively high mass-loss rate during creation of the shell. Based on the expansion velocity, the age of the shell is 2300 yr, over which the mass-loss rate has slowly decreased by an order of magnitude. This is consistent with the hydrodynamical modelling of the observed spiral shape seen in the 12CO(3−2) maps (Maercker et al. 2012). Hence, employing two different and independent methods of analysis (detailed hydrodynamical modelling of the structure seen in one transition vs. radiative transfer of the overall emission in all three transitions), we arrive at the same conclusion. The models form a shell during a TP, with a subsequent linear decline of the mass-loss rate to the present-day value. Assuming a TP mass-loss rate of 2.3 × 10-5 M yr-1 for 200 yr and a linear decline to the present-day value of 10-6 M yr-1 over an additional 2100 yr, the total mass lost by R Scl since the onset of the most recent TP is 0.03 M. If the mass-loss rate instead had evolved according to the classical scenario (i.e. with a sudden drop after the TP), the total mass lost would only have been 0.007 M.

As the total amount of mass lost during the TP cycle increases monotonically during AGB evolution, the determined mass can be used to roughly estimate the evolutionary stage of R Scl, depending on the (unknown) main-sequence mass. For a 3 M star (main-sequence mass) at solar metallicity typical inter-pulse timescales once the third dredge-up has set in are 60 000 yr. Using the values derived for R Scl, and assuming that the present-day mass-loss rate remains constant for the remainder of the TP cycle at 10-6 M yr-1, this implies that up to 0.09 M will be lost in total during the most recent TP cycle, placing R Scl at the end of the TP-AGB (Karakas & Lattanzio 2007). A 4.5 M star (main-sequence mass) on the other hand has typical inter-pulse timescales of 10 000 yr. In this case only a total of 0.04 M will be lost in the most recent TP cycle, and R Scl would have only evolved about halfway along the TP-AGB (Karakas & Lattanzio 2007).

Our results show that a significant fraction of the mass during a TP cycle will be lost immediately after the pulse due to a relatively slow decline from the thermal-pulse mass-loss rate. The total amount of mass lost during the TP-cycle limits the lifetime on the AGB and hence the number of TPs a star can experience. The mass of the stellar hydrogen envelope will also have a profound effect on the nucleosynthetic processes inside the star (e.g. hot bottom burning). The evolution of the mass-loss rate throughout the TP-cycle therefore also strongly affects the chemical evolution of the star, and the enrichment of the CSE and ISM.

5. Conclusions

We present the full set of ALMA Cycle 0 observations of 12CO towards the carbon AGB star R Scl. The observations clearly resolve the shell around R Scl and reveal a spiral structure induced by a binary companion. The data allow us to separate the shell from the extended emission inside the shell and analyse both components separately. Radiative transfer modelling of the shell and the present-day mass loss constrains the mass in the shell and average mass-loss rate since the formation of the shell. The results are consistent with a shell creation during a TP with a subsequent decline of the mass-loss rate. In particular we find that

  • contrary to what was believed so far, the shell aroundR Scl is entirely filled with gas and as such is notdetached,

  • the shell is consistent with an increase in mass-loss rate and expansion velocity during a TP, leading to a two-wind interaction with a previous, slower wind,

  • the estimated shell mass-loss rate is 2.3 × 10-5 M yr-1 for a period of 200 yr, while the post-pulse mass-loss rate is on average 1.6 × 10-5 M yr-1 during the last 2100 yr, and goes at least as low as 3.5 × 10-6 M yr-1 in recent years,

  • the derived mass-loss rates imply that the decline in mass-loss rate after the pulse must have been significantly slower than previously assumed, and

  • the amount of mass lost during a TP cycle may be significantly higher than previously assumed, strongly affecting the lifetime on the AGB, and the chemical evolution of the star, CSE, and ISM.

Additionally, we observe a higher-velocity component centred on the star for which we cannot find an obvious explanation. ALMA Cycle 2 observations at high-angular resolution will give a more complete picture of the spiral structure close to the star and include ACA observations to recover also the extended flux. The data will be essential for deriving a more accurate mass-loss rate evolution since the creation of the shell and will allow us to effectively constrain hydrodynamical models.


1

Note that Vlemmings et al. (2013) estimate that only 25% of the flux is recovered for the 12CO(3−2) line. This is however due to an erroneous main-beam correction of the APEX data in De Beck et al. (2010).

Acknowledgments

This paper makes use of ALMA data from project No. ADS/ JAO.ALMA#2011.0.00131.S. ALMA is a partnership of ESO (representing its member states), the NSF (USA) and NINS (Japan), together with the NRC (Canada) and NSC and ASIAA (Taiwan), in cooperation with the Republic of Chile. The Joint ALMA Observatory is operated by ESO, AUI/NRAO and NAOJ. M.M. has received funding from the People Programme (Marie Curie Actions) of the EU’s FP7 (FP7/2007-2013) under REA grant agreement No. 623898.11. W.V. acknowledges support from Marie Curie Career Integration Grant 321691 and ERC consolidator grant 614264. F.K. and M.B. acknowledge funding by the Austrian Science Fund FWF under project number P23586. M.B. further acknowledges funding through the ESO Director General’s Discretionary Fund and the uni:docs fellowship of the University of Vienna. H.O. acknowledges financial support from the Swedish Research Council.

References

  1. Bladh, S., Höfner, S., Aringer, B., & Eriksson, K. 2015, A&A, 575, A105 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  2. Cox, N. L. J., Kerschbaum, F., van Marle, A.-J., et al. 2012, A&A, 537, A35 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  3. De Beck, E., Decin, L., de Koter, A., et al. 2010, A&A, 523, A47 [Google Scholar]
  4. González Delgado, D., Olofsson, H., Schwarz, H. E., Eriksson, K., & Gustafsson, B. 2001, A&A, 372, 885 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  5. González Delgado, D., Olofsson, H., Schwarz, H. E., et al. 2003, A&A, 399, 1021 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  6. Herwig, F. 2005, ARA&A, 43, 435 [NASA ADS] [CrossRef] [Google Scholar]
  7. Izumiura, H., Waters, L. B. F. M., de Jong, T., et al. 1997, A&A, 323, 449 [NASA ADS] [Google Scholar]
  8. Izumiura, H., Ueta, T., Yamamura, I., et al. 2011, A&A, 528, A29 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  9. Karakas, A., & Lattanzio, J. C. 2007, PASA, 24, 103 [NASA ADS] [CrossRef] [Google Scholar]
  10. Kerschbaum, F., Ladjal, D., Ottensamer, R., et al. 2010, A&A, 518, L140 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  11. Knapp, G. R., Pourbaix, D., Platais, I., & Jorissen, A. 2003, A&A, 403, 993 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  12. Lambert, D. L., Gustafsson, B., Eriksson, K., & Hinkle, K. H. 1986, ApJS, 62, 373 [NASA ADS] [CrossRef] [Google Scholar]
  13. Lindqvist, M., Olofsson, H., Lucas, R., et al. 1999, A&A, 351, L1 [NASA ADS] [Google Scholar]
  14. Mackey, J., Mohamed, S., Gvaramadze, V. V., et al. 2014, Nature, 512, 282 [NASA ADS] [CrossRef] [Google Scholar]
  15. Maercker, M., Olofsson, H., Eriksson, K., Gustafsson, B., & Schöier, F. L. 2010, A&A, 511, A37 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  16. Maercker, M., Mohamed, S., Vlemmings, W. H. T., et al. 2012, Nature, 490, 232 [NASA ADS] [CrossRef] [PubMed] [Google Scholar]
  17. Maercker, M., Ramstedt, S., Leal-Ferreira, M. L., Olofsson, G., & Floren, H. G. 2014, A&A, 570, A101 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  18. Mamon, G. A., Glassgold, A. E., & Huggins, P. J. 1988, ApJ, 328, 797 [NASA ADS] [CrossRef] [Google Scholar]
  19. Mattsson, L., Höfner, S., & Herwig, F. 2007, A&A, 470, 339 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  20. Mečina, M., Kerschbaum, F., Groenewegen, M. A. T., et al. 2014, A&A, 566, A69 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  21. Olofsson, H., Eriksson, K., & Gustafsson, B. 1988, A&A, 196, L1 [NASA ADS] [Google Scholar]
  22. Olofsson, H., Carlstrom, U., Eriksson, K., Gustafsson, B., & Willson, L. A. 1990, A&A, 230, L13 [NASA ADS] [Google Scholar]
  23. Olofsson, H., Eriksson, K., Gustafsson, B., & Carlstrom, U. 1993, ApJS, 87, 267 [NASA ADS] [CrossRef] [Google Scholar]
  24. Olofsson, H., Bergman, P., Eriksson, K., & Gustafsson, B. 1996, A&A, 311, 587 [NASA ADS] [Google Scholar]
  25. Olofsson, H., Bergman, P., Lucas, R., et al. 2000, A&A, 353, 583 [NASA ADS] [Google Scholar]
  26. Olofsson, H., Maercker, M., Eriksson, K., Gustafsson, B., & Schöier, F. 2010, A&A, 515, A27 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  27. Olofsson, H., Bergman, P., & Lindqvist, M. 2015, A&A, 582, A102 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  28. Ramstedt, S., Maercker, M., Olofsson, G., Olofsson, H., & Schöier, F. L. 2011, A&A, 531, A148 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  29. Schneider, R., Valiante, R., Ventura, P., et al. 2014, MNRAS, 442, 1440 [NASA ADS] [CrossRef] [Google Scholar]
  30. Schöier, F. L., & Olofsson, H. 2001, A&A, 368, 969 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  31. Schöier, F. L., Lindqvist, M., & Olofsson, H. 2005, A&A, 436, 633 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  32. Stanek, K. Z., Knapp, G. R., Young, K., & Phillips, T. G. 1995, ApJS, 100, 169 [NASA ADS] [CrossRef] [Google Scholar]
  33. Steffen, M., & Schönberner, D. 2000, A&A, 357, 180 [NASA ADS] [Google Scholar]
  34. Steffen, M., Szczerba, R., & Schoenberner, D. 1998, A&A, 337, 149 [NASA ADS] [Google Scholar]
  35. van der Veen, W. E. C. J., & Habing, H. J. 1988, A&A, 194, 125 [NASA ADS] [Google Scholar]
  36. Vassilev, V., Meledin, D., Lapkin, I., et al. 2008, A&A, 490, 1157 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  37. Vassiliadis, E., & Wood, P. R. 1993, ApJ, 413, 641 [NASA ADS] [CrossRef] [Google Scholar]
  38. Vlemmings, W. H. T., Maercker, M., Lindqvist, M., et al. 2013, A&A, 556, L1 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  39. Waters, L. B. F. M., Loup, C., Kester, D. J. M., Bontekoe, T. R., & de Jong, T. 1994, A&A, 281, L1 [NASA ADS] [Google Scholar]
  40. Whitelock, P. A., Feast, M. W., & van Leeuwen, F. 2008, MNRAS, 386, 313 [NASA ADS] [CrossRef] [Google Scholar]

All Tables

Table 1

Summary of the reduced image cubes of the ALMA observations of the circumstellar environment of R Scl.

Table 2

Summary of ALMA observations of the circumstellar environment of R Scl.

Table 3

Summary of single-dish (SD) observations towards R Scl.

All Figures

thumbnail Fig. 1

ALMA observations of 12CO(1−0) towards R Scl. The bin size of each panel is 1.5 km s-1. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner.

In the text
thumbnail Fig. 2

ALMA observations of 12CO(2−1) towards R Scl. The bin size of each panel is 1.0 km s-1. Panels with a spacing of 2 km s-1 are shown. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner.

In the text
thumbnail Fig. 3

ALMA observations of 12CO(3−2) towards R Scl. The bin size of each panel is 0.5 km s-1. Panels with a spacing of 1.5 km s-1 are shown. The color scale is given in Jy/beam. The beam ellipse is given in the lower left corner. These data were first presented in Maercker et al. (2012).

In the text
thumbnail Fig. 4

SD observations towards R Scl (from left to right): SEST CO(1–0), IRAM 30 m CO(1–0), APEX CO(2–1), and APEX CO(3–2). The FWHM of the SD beams are 44′′, 22′′, 27′′, and 18′′, respectively. The red spectra show the ALMA observations of the respective transitions convolved with Gaussian beams to give the FWHM from the respective telescopes.

In the text
thumbnail Fig. 5

Qualitative analysis of the effect of extended emission on the ALMA Cycle 0 observations of ALMA. The left columns shows toy-models of the emission from the shell around R Scl and extended emission inside the shell at the νLSR\hbox{$\varv_{\rm{LSR}}^*$} for the 12CO(1−0), 12CO(2−1), and 12CO(3−2) transitions (top to bottom, respectively). The right column shows the resulting simulated observations using the ALMA Cycle 0 compact configuration of the main array (simulated using the CASA simulator).

In the text
thumbnail Fig. 6

ALMA 12CO observations of the shell for 12CO(1−0), 12CO(2−1), and 12CO(3−2) (black lines, panels 1–3, respectively). The data are extracted from annuli within ±3′′ from the projected radius of the shell in each velocity bin in the images smoothed to 4′′ resolution. For comparison, the black dotted lines show the emission integrated over the entire image for each velocity bin instead (i.e. also containing emission from the CSE). The red lines show the best-fit model of the shell only. The right panel shows the χ2 map of the radiative transfer models of the shell with shell-mass vs. shell temperature. The colour scale gives the χ2 value, the white cross indicates the best-fit model. The white contours give the 1σ and 2σ levels (the 3σ contours fall outside of the plotted range).

In the text
thumbnail Fig. 7

Top: SD spectra (black, from left to right: SEST 12CO(1−0), IRAM 12CO(1−0), APEX 12CO(2−1), and APEX 12CO(3−2)) with the best-fit shell model convolved with the respective beams (red). The green spectra show the shell emission extracted from the ALMA data and convolved with the respective SD beams. Bottom: SD spectra after subtracting the best-fit shell models. The red lines show the best-fit model fit to the shell-subtracted SD observations to constrain the average mass-loss rate since creation of the shell.

In the text

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