The Molecular Outflow in NGC 253 at a Resolution of Two Parsecs

, , , , , , , , , , , and

Published 2019 August 12 © 2019. The American Astronomical Society. All rights reserved.
, , Citation Nico Krieger et al 2019 ApJ 881 43 DOI 10.3847/1538-4357/ab2d9c

Download Article PDF
DownloadArticle ePub

You need an eReader or compatible software to experience the benefits of the ePub3 file format.

0004-637X/881/1/43

Abstract

We present 0farcs15 (∼2.5 pc) resolution ALMA CO(3–2) observations of the starbursting center in NGC 253. Together with archival ALMA CO(1–0) and CO(2–1) data, we decompose the emission into disk and nondisk components. We find ∼7%–16% of the CO luminosity to be associated with the nondisk component (1.2–4.2 × 107 K km s−1 pc2). The total molecular gas mass in the center of NGC 253 is ∼3.6 × 108 M with ∼0.5 × 108 M (∼15%) in the nondisk component. These measurements are consistent across independent mass estimates through three CO transitions. The high-resolution CO(3–2) observations allow us to identify the molecular outflow within the nondisk gas. Using a starburst conversion factor, we estimate the deprojected molecular mass outflow rate, kinetic energy, and momentum in the starburst of NGC 253. The deprojected molecular mass outflow rate is in the range of ∼14–39 M yr−1 with an uncertainty of 0.4 dex. The large spread arises due to different interpretations of the kinematics of the observed gas while the errors are due to unknown geometry. The majority of this outflow rate is contributed by distinct outflows perpendicular to the disk, with a significant contribution by diffuse molecular gas. This results in a mass-loading factor $\eta ={\dot{M}}_{\mathrm{out}}/{\dot{M}}_{\mathrm{SFR}}$ in the range η ∼ 8−20 for gas ejected out to ∼300 pc. We find the kinetic energy of the outflow to be ∼2.5–4.5 × 1054 erg and a typical error of ∼0.8 dex, which is ∼0.1% of the total or ∼8% of the kinetic energy supplied by the starburst. The outflow momentum is 4.8–8.7 × 108 M km s−1 (∼0.5 dex error) or ∼2.5%–4% of the kinetic momentum released into the ISM by the feedback. The unknown outflow geometry and launching sites are the primary sources of uncertainty in this study.

Export citation and abstract BibTeX RIS

1. Introduction

Outflows driven by star formation are thought to be a crucial driver of galaxy evolution. Strong stellar feedback caused by high star formation rate (SFR) densities can launch outflows of ionized, neutral, and molecular gas that can potentially escape the main body of a galaxy. Consequently, such outflowing gas removes the potential fuel for future star formation. Therefore, outflows can suppress and quench star formation, as also demonstrated by theoretical predictions and simulations (e.g., Dekel & Silk 1986; Krumholz et al. 2017; Ma et al. 2018). Depending on the velocity of the outflow and a galaxy's escape velocity, outflowing gas can be reaccreted at later cosmic times (the so-called "galactic fountain") or leave the system altogether. This process thus has the potential to enrich the galactic disk and circumgalactic medium with heavy metals (e.g., Oppenheimer & Davé 2006; Oppenheimer et al. 2010; Hopkins et al. 2012; Christensen et al. 2018).

Galactic outflows are a multiphase phenomenon and are observed across the electromagnetic spectrum from X-ray (e.g., Strickland & Heckman 2007), UV (e.g., Hoopes et al. 2005), optical like Hα (e.g., Westmoquette et al. 2009), to IR (e.g., Veilleux et al. 2009), cold dust (e.g., Roussel et al. 2010), PAH emission (e.g., Engelbracht et al. 2006), and submillimeter to radio including H i (e.g., Bolatto et al. 2013; Leroy et al. 2015b; Lucero et al. 2015). Typically, large-scale outflow features at high relative velocity (hundreds to thousands of km s−1) are observed in the ionized and neutral gas, whereas molecular outflows often appear as smaller, more compact features (Strickland et al. 2002; Westmoquette et al. 2011). The latter are nonetheless important as they dominate the mass budget (Leroy et al. 2015b). In some galaxies, the gas phases seem to be stratified with an inner ionized outflow cone, a surrounding neutral shell, and molecular gas situated along the outer edge (e.g., Meier et al. 2015) Typically, the outflows originate from an extended region, so the apparent outflow cone has its tip cut off.

Molecular outflows are thus closely intertwined with feedback processes and star formation. The high-resolution structure and kinematic properties of (molecular) outflows have not been studied in great detail yet, primarily due to the lack of high-resolution and -sensitivity observations. Starburst galaxies are the obvious target to study star-formation-driven outflows due to the high SFR in these systems. Consequently, molecular outflows have been studied over the past years in a few nearby starbursts: M82 (Walter et al. 2002; Leroy et al. 2015b), NGC 253 (Bolatto et al. 2013; Walter et al. 2017; Zschaechner et al. 2018), NGC 1808 (Salak et al. 2018), and ESO320-G030 (Pereira-Santaella et al. 2016).

NGC 253 is one of the nearest starburst systems at a distance of 3.5 Mpc (Rekola et al. 2005). It is considered one of the prototypical starburst galaxies with an SFR surface density of ΣSFR ∼ 102 M yr−1 kpc−2 in the nuclear region and a molecular depletion time that is ${\tau }_{\mathrm{dep}}^{\mathrm{mol}}\sim 5\mbox{--}25$ times lower than what is found in local disks (Leroy et al. 2015a). A galactic wind emerges from the central ∼200 pc of NGC 253, which has been characterized in Hα, X-ray, as well as neutral and molecular gas emission (e.g., Turner 1985; Heckman et al. 2000; Strickland et al. 2000, 2002; Sharp & Bland-Hawthorn 2010; Sturm et al. 2011; Westmoquette et al. 2011; Bolatto et al. 2013; Walter et al. 2017). Due to the close proximity, starburst and galactic winds can be studied in detail and individual structures can be resolved.

Studies of the molecular gas phase in NGC 253 showed that its central starburst is fueled by gas accretion along the bar (Paglione et al. 2004). The molecular ISM in the nuclear region is structured in several clumps that show high temperatures of ∼50 K (Paglione et al. 2004; Sakamoto et al. 2011; Mangum et al. 2019). From earlier low-resolution observations (>20 pc, e.g., Sakamoto et al. 2006, 2011) to recent observations at high resolution (8 pc × 5 pc in Ando et al. 2017 and 2 pc in Leroy et al. 2018), the number of molecular clumps associated with the starburst has increased from ∼5 to 14. These studies find the clumps to be massive (4–10 × 104 M), compact (<10 pc), chemically rich (up to >19 molecules detected in the 0.8 mm band), and hot (up to 90 K). Each clump likely hosts an embedded massive star cluster (Leroy et al. 2018). Further structures in the molecular gas are shells and bubbles blown up by feedback from the intense star formation process. Sakamoto et al. (2006) found two 100 pc diameter superbubbles. Bolatto et al. (2013) reported molecular streamers11 originating from these shells with a lower limit on the outflow rate of 3–9 M yr−1, about three times the SFR. This estimate was revisited by Zschaechner et al. (2018), based on observations that show that the CO emission associated with the most prominent streamer is optically thick, increasing it to 25–50 M yr−1.

As suggested by these studies, the outflow rate in NGC 253 is factors of a few to potentially >10 larger than the SFR. Hence, the impact of the outflows on the amount of material lost from the molecular gas reservoir, and thus the lifetime of the starburst, is significant. The availability of new data makes it interesting to revisit the determination of the mass outflow rate in NGC 253, while also removing some limitations of previous determinations. Bolatto et al. (2013) estimated the outflow rate from a few massive molecular streamers, but did not include potential diffuse outflowing gas. Also, resolution plays an important role in the ability to disentangle outflows from material in the starbursting disk. New ALMA band 7 observations provide excellent spatial resolution and reasonable surface brightness sensitivity. This information enables increasingly accurate determination of the total mass outflow rate and its impact on the starburst.

In this work, we present ALMA CO(3–2) observations carried out in cycles 3 and 4 that target the molecular gas in the central ∼750 pc of NGC 253. Together with ancillary band 3 and 6 data from our previous works (Bolatto et al. 2013; Leroy et al. 2015a; Meier et al. 2015; Zschaechner et al. 2018), we have an inventory of three CO lines to study the molecular gas in the starbursting disk and a kinematically different component that includes the outflow. By decomposing the detected emission, we aim to measure the total molecular gas outflow rate in NGC 253 and improve upon previous less systematic results.

Throughout this paper, we adopt a distance of 3.5 Mpc to NGC 253 (Rekola et al. 2005) at which 1'' corresponds to 17 pc. We also define the "center" of the nuclear region of NGC 253 to be the kinematic center at α, δ = 00h47m33fs134, −25°17m19fs68, as identified in Müller-Sánchez et al. (2010). The paper is structured as follows: in Section 2, we describe observational setup and data reduction, and show the results in the form of channel maps, moment maps, and position–velocity (pV) diagrams. Our approach to separating gas in the star-forming disk from potentially outflowing gas is laid out in Section 3. Section 4 discusses the derived quantities such as the CO luminosities, molecular gas masses, outflow rates, kinetic energies, and momenta. Our conclusions are summarized in Section 5.

2. Data Reduction and Imaging

2.1. Data Reduction

The data presented in this paper are based on observations in ALMA cycles 2, 3, and 4 in bands 3, 6, and 7 that cover the redshifted emission in NGC 253 of CO(1–0), CO(2–1), and CO(3–2), as well as other molecular lines. For the data reduction and imaging of band 3 and 6 data, see Bolatto et al. (2013), Leroy et al. (2015a), Meier et al. (2015), and Zschaechner et al. (2018). Table 1 gives an overview of the data sets used in this analysis.

Table 1.  Details of the Data Sets Used in This Analysis

  CO(1–0) CO(2–1) CO(3–2)
ALMA ID 2011.1.00172.S 2012.1.00108.S 2015.1.00274.S
Spatial Resolution 1farcs85 × 1farcs32 1farcs70 × 1farcs02 0farcs17 × 0farcs13
  31.4 pc × 22.4 pc 28.8 pc × 17.3 pc 2.9 pc × 2.2 pc
Spectral Resolution 5.0 km s−1 5.0 km s−1 2.5 km s−1
rms Noise Per Channel 1.99 mJy beam−1 2.19 mJy beam−1 0.81 mJy beam−1
  75 mK 29 mK 0.37 K

Download table as:  ASCIITypeset image

For the band 7 observations, we tuned the lower sideband to 342.0–345.8 GHz and the upper sideband to 353.9–357.7 GHz (total bandwidth 7.6 GHz) with a 976.6 kHz channel width (corresponding to 0.8 km s−1). We targeted the central ∼750 pc of NGC 253 in a linear four-pointing mosaic with two configurations of the 12 m array (12 m compact and 12 m extended, half-power beam width ∼30'') and a five-pointing mosaic of the 7 m array (ACA, half-power beam width ∼50''). Additional single-dish observations with the total power array (TP) recovers emission on large spatial scales. The baseline ranges covered by this setup are 8.9–49.0 m, 15.1–783.5 m, and 15.1–1813.1 m for the ACA and the two 12 m setups, respectively.

The observations were carried out primarily in the first half of 2016 (TP: 2015 December 7 to 2016 August 2; ACA: 2015 December 7 to 2016 November 23; 12 m compact configuration: 2016 April 16, 2016 April 23, 2016 June 17, 2016 June 27; 12 m extended configuration: 2016 August 30, 2016 September 3). The total on-source observation time is 48 hr and 45 minutes split across 27 hr and 23 minutes (TP), 14 hr and 57minutes (ACA), 2 hr and 37 minutes (12 m compact), and 3hr and 59 minutes (12 m extended). The calibrators were J0006–0623 (bandpass); J0038–2459 (complex gain); the asteroid Pallas (absolute flux density); and J0104–2416 and J0106–2718 (both WVR). Visibilities of the 12 m data are calibrated using the ALMA cycle 3 pipeline in casa 4.6.0 and the delivered calibration script. The other data sets are calibrated in casa 4.7.2 and the cycle 4 pipeline.

In order to image the spectral lines, we subtract the continuum in the (U, V) plane using a first-order polynomial fitted to the channels that do not contain strong spectral lines. We reliably detect >25 lines in the range 342.0–345.0 GHz and 353.9–357.7 GHz aside from the four strong lines CO(3–2), HCN4–3), HCO+(4–3), and CS(7–6). Most of these lines are weak and only detected in small spatial regions so they do not affect the overall continuum fit and subtraction.

2.2. Imaging

Combined imaging of the interferometric data is done with the tclean task in casa 5.4.0, which includes crucial bug fixes for ALMA mosaics.12 We regrid the visibilities during deconvolution to a spectral resolution of 2.5 km s−1. Applying a Briggs weighting scheme with robust parameter 0.5 results in a synthesized beam of 0farcs17 × 0farcs13 (pixel scale 0farcs05). The images are cleaned to a level of 2.5× the rms noise in line-free channels of 2.5 × 0.81 mJy beam−1 (2.5 × 0.37 K) using a clean mask derived from a low-resolution image of the compact 12 m array CO(3–2) data only.

We correct the cleaned images for the mosaic sensitivity pattern (mosaic primary beam response pattern), combine them with the TP images using feather, and finally convert the units to brightness temperature.

For the final images, we do not consider the ACA data as they introduce large-scale noise fluctuations toward the edge of the mosaic, which we attribute to decreasing sensitivity of the 12 m data relative to the ACA data. These fluctuations obscure the regions where outflows were previously found. This work requires accurate integrated flux measurements and correct representation of the small-scale structure, which are defined by single-dish observations (TP) and long baselines (extended 12 m), respectively. By checking the images without ACA data against the images including ACA data, we can confirm that neither the overall flux scale nor the small-scale structure is significantly altered.

Data products for CO(1–0) are shown in Bolatto et al. (2013), Meier et al. (2015), and Leroy et al. (2015a), and Zschaechner et al. (2018) present the CO(2–1) data. Imaging results for CO(3–2) are presented in the following section.

In order to keep the amount of detail and contrast in the high-resolution data, we do not match the spatial resolution to that of the data with the lowest resolution, but perform our analysis at the native resolution of each data set. All further steps work on the data cubes masked at 5.0σ (see Table 1) and further masks where necessary. To generate the masks, we do not consider the nonuniform noise level caused by the mosaic sensitivity pattern but use the per-channel rms noise in the center of the field of view.

2.3. CO(3–2) Data Presentation

In this section, we present the CO(3–2) data in different representations. Channel maps (Figure 1), moment maps (Figure 2), and a pV diagram (Figure 3) show the spatial and kinematic structures to be discussed and highlight the data quality.

Figure 1.

Figure 1. Channel maps of CO(3–2) in NGC 253. Every 16th channel of 2.5 km s−1 width is shown with the corresponding line-of-sight velocity (vsys = 250 km s−1) given in the upper-right corner of each panel. The synthesized beam of 0farcs17 × 0farcs13 is plotted in the lower-right corner; it is hardly noticeable due to its small size. Contours are plotted at 10σ, 20σ, 40σ, and 80σ with an rms noise of σ = 0.37 K. Large structures are marked by dashed contours in those panels that show them most clearly. Further new shells are indicated by dashed circles.

Standard image High-resolution image
Figure 2.

Figure 2. CO(3–2) moment maps of NGC 253. Top: integrated intensity map (moment 0); contours are shown from 250 to 8000 K km s−1 in factors of 2. Middle: velocity field (moment 1); contours are shown from 100 to 400 km s−1 in steps of 50 km s−1. Bottom: moment 2 (corresponding to the velocity dispersion if the line profile were Gaussian); contours are shown from 0 to 100 km s−1 in steps of 20 km s−1. The color scale is chosen to saturate a few regions with dispersions >100 km s−1. All maps are generated from the data cube masked at 5σ threshold per channel and confined to the collapsed clean mask to include only emission that has been processed by the clean algorithm.

Standard image High-resolution image
Figure 3.

Figure 3. CO(3–2) position–velocity diagram of NGC 253 along the major axis centered on the kinematic center averaged over the full width of the field of view (∼30''). Pixels below 3σ are masked and contours are drawn at 10σ, 20σ, 40σ, 80σ with an rms noise of σ = 0.37 K. Note the vertical spikes indicating high-velocity dispersion due to outflowing gas.

Standard image High-resolution image

Figure 1 shows channel maps of the image cube. To retain the intrinsic resolution, only every 16th channel (40 km s−1 spacing) is shown here. Aside from the rotating disk of molecular gas, we clearly detect the prominent southwest (SW) streamer (Walter et al. 2017) in the range 180–250 km s−1 (Figure 1, panels 220 and 260 km s−1). Additional gas streamers are apparent between ∼60 and ∼350 km s−1 toward the north and south of the disk, as can be seen, for example, in the panels at 260 or 340 km s−1. Several notable molecular shells are present between 180 and 340 km s−1. Aside from the (super)shells at the eastern (left) and western (right) edges of the map that were previously identified by Sakamoto et al. (2006) and Bolatto et al. (2013), further smaller shell-like structures are located along the molecular disk.

We calculate image moments (Figure 2) with immoments in casa for emission above 5σ for the moment 0 (integrated intensity), moment 1 (intensity-weighted line-of-sight velocity), and moment 2 (intensity-weighted velocity dispersion) maps. Note that due to the complex line shapes, the moment 2 map does not directly correspond to velocity dispersion, which is only the case for Gaussian line profiles. The maps are further constrained to the region defined by the collapsed clean mask to limit them to emission that has been processed by the clean algorithm.

Figure 3 shows the kinematic structure of NGC 253 in a pV diagram along the major axis of the disk (PA = 55°) averaged over the full width of the field of view (∼30'') centered on the kinematic center. The pV cut shows several high-velocity dispersion structures extending from a rotating disk, indicative of outflows.

3. Separating Disk and Nondisk Emission

3.1. Separating Disk and Nondisk Emission in Position–Position–Velocity (ppV) Space

Our goal is to account for all molecular wind, separating outflowing molecular gas from foreground or background disk emission. A clean separation in 2D position–position space cannot be easily accomplished, due to the inclination of 78° of NGC 253. At this high inclination, outflows and disk emission are cospatial in projection. Kinematic information from line-of-sight velocities, however, makes it possible to disentangle the outflow. Note that this becomes increasingly difficult as the velocity vector aligns with the plane of the sky, resulting in line-of-sight velocities that are systemic. From Hα kinematic modeling, the NGC 253 outflow is approximately biconical with an axis normal to the disk and an opening angle of ∼60° (Westmoquette et al. 2011), and thus the range of possible projection angles is large (see Meier et al. 2015 for a sketch). Note that because the cone-opening angle is larger than the angle between the axis of the cone and the plane of the sky, gas in the approaching and receding cones can have both blue- and redshifted velocities with respect to systemic.

The launching of molecular gas occurs within the disk through star formation feedback, thus the outflows originate from the same location in ppV space as disk molecular clouds. Outflows will therefore blend into the disk near their launching sites, which makes disentanglement increasingly difficult closer to the starburst region.

The complexity of systematically separating the emission corresponding to the disk and the outflow in ppV space is challenging. Algorithmically, this separation is simpler in lower dimensional space, obtained by slicing the data cube into a collection of 2D pV diagrams. In what follows, we identify kinematic components in these diagrams, which we then project back to 3D ppV space. In order to avoid introducing biases, we model the large-scale disk velocity field and use this model as the basis of the kinematic separation.

3.2. Definition of Components

Images of the center of NGC 253 on large scales show an elongated gas structure (Figure 2 top) with a regular velocity field (Figure 2 middle) that roughly matches a rotating disk disturbed by streaming motions from a bar (e.g., Paglione et al. 2004). The elongated gas structure is consistent with a highly inclined disk of molecular gas, or possibly a ring-like structure as observed in other galaxies (for example, NGC 1512, NGC 1808; Salak et al. 2016; Ma et al. 2018). Similar structures break up at higher spatial resolution into two embracing spiral arms or complex nonclosed orbits in the Milky Way center (Krumholz & Kruijssen 2015; Henshaw et al. 2016; Sormani et al. 2018).

Superimposed on this large-scale structure are smaller features that are not part of the large-scale pattern of rotation and streaming motions. Some of them have high aspect ratios in channel maps and line-of-sight velocity gradients, both typical for outflows. Local deviations from the large-scale velocity field can also be due to infalling gas, or clumps of gas that do not follow the global pattern, due perhaps to cloud–cloud collision.

Henceforth, we will refer to the bulk of the molecular gas that moves according to the large-scale velocity field in the central regions of NGC 253 as the disk. We assume that this large-scale velocity field consists of rotation and streaming motions. The term nondisk refers to any gas that is not following the ppV structure of the disk. By this definition, nondisk gas encompasses material from features that may be attributed to a variety of physical processes, including outflow and infall.

Structures of outflowing gas are frequently referred to by names that describe their kinematic or spatial appearance, such as "streamer." We will use the term outflow to denote localized structures with morphology and kinematics consistent with gas moving away from the disk, as inferred from their location in ppV space. Typical signatures are a velocity that is inconsistent with rotation in the plane of the disk and a high aspect ratio oriented roughly perpendicular to the disk major axis. Note that similar kinematic and structural properties can arise in infalling gas clouds. We will assume that all molecular gas with these characteristics is outflowing, which is likely the case for the majority of the material in NGC 253.

3.3. Position–Velocity Slicing

Kinematic analyses typically depend on high signal-to-noise ratios (S/N) because faint features can easily drown in noisy spectra. As a trade-off between necessarily high S/N and also trying to include as much faint emission as possible, we conduct the following analysis on data cubes masked at the 5σ level (see Table 1).

We split the ppV cubes into pV slices along the major axis of NGC 253 as shown in Figure 4. The slices assume the kinematic center is α, δ = 00h47m33fs134, −25°17m19fs68 (Müller-Sánchez et al. 2010), and are oriented along the major axis of the projected CO emission with PA = 55°. The area sliced is chosen to cover the region for which we have overlapping CO(1–0), (2–1), and (3–2), and also cover the full length of the SW streamer outflow feature (17farcs5; Walter et al. 2017).

Figure 4.

Figure 4. Size and orientation of the position–velocity slices overlaid on the integrated intensity image of CO(1–0) (top), CO(2–1) (middle), and CO(3–2) (bottom). Each slice is 5farcs0 wide and overlaps adjacent slices by 2farcs5.

Standard image High-resolution image

These requirements are fulfilled by slices of 50'' (850 pc) length (major axis) and covering 50'' (850 pc) along the minor axis (Figure 4). To reduce the problems introduced by splitting features across slices, each slice is 5farcs0 (85 pc) wide, and we overlap slices by half their width (2farcs5, 42 pc). A sample pV diagram is shown in Figure 5 for the central slice, which runs along the major axis (offset 0farcs0). A complete set of pV diagrams is given in Appendix C. The resolution differences between our three transitions, a factor of ∼100 in beam solid angle, are apparent in Figure 5. In the high angular resolution CO(3–2), small features with large line widths are common. These features are blurred out in the lower resolution CO(1–0) and (2–1).

Figure 5.

Figure 5. Position–velocity diagram of the central slice (offset 0farcs0) showing the construction of the disk/nondisk masks. The background images show the flux density above 5.0σ for CO(1–0) (top), CO(2–1) (center), and CO(3–2) (bottom) on identical gray scales. Contours are drawn at 1, 2, 4, 8 and 16 K. The central velocity for our model of the disk emission is illustrated by the red line. The golden-shaded area denotes the disk mask. Similar figures for other offsets are shown in Appendix C. Note that the different transitions have different angular resolutions.

Standard image High-resolution image

3.4. Modeling the Disk

We derive a model for the velocity of the disk component from the CO(1–0) observations using the kinematic fitting tool diskfit (Spekkens & Sellwood 2007; Sellwood & Sánchez 2010; Sellwood & Spekkens 2015). Because the CO(1–0) observations cover the largest area among our observations, we use them to derive the model; the additional information provided by the CO(2–1) and/or CO(3–2) data is negligible in terms of the bulk motions of the gas. We obtain a CO(1–0) velocity field by computing the first moment of the cube after masking it at 20σ (1.26 K), in order to represent the velocity of the bright emission. We show the details of the fit parameters and a comparison to the CO(1–0) velocity field in Appendix A.

In each pV slice, we use the velocity profile of the diskfit model to define the local disk velocity. We consider the CO emission to be consistent with the disk component of the emission when the velocity difference is within the local observed velocity range, Δv. This velocity range varies spatially and depends on the distance x from the major axis, increasing toward the center due to the combined effects of higher intrinsic velocity dispersion and projection. For the success of this analysis, it is crucial that Δv is broad enough to cover the observed velocity range of the disk but also narrow enough in order to not classify potential outflows as a disk. The definition of Δv is thus a crucial source of uncertainty for the derived quantities. We parameterize the velocity range of the disk as

Equation (1)

with Δv in km s−1 and x in arcseconds. We find this empirical relation to fit the pV data best, and small variations of order 10%–20% already show a noticeable mismatch as discussed in Appendix B. The quality of this definition can be assessed from Figure 5 and Appendix C: the velocity ranges are wide enough to include obvious emission of the disk but do not extend into the kinematically distinct features (potential outflows) that appear as spikes. This is most apparent for CO(3–2) as this line offers the highest spatial resolution. The effect of a 10% change in the velocity range Δv corresponds to up to 0.1 dex variations in the derived quantities (see Appendix B).

3.5. Selecting the Components

We use the modeled velocity field and the Δv relation together to define a "disk mask" over ppV space, corresponding to emission that is consistent with disk rotation. We show in Figure 5 the central pV slices for CO(1–0), (2–1), and (3–2). We show in Appendix C the complete set of pV slices.

Note that the CO emission extends beyond the disk mask. These extensions are not symmetric and due to nondisk gas and projection effects. At ∼78° inclination, gas flowing perpendicular to the galaxy disk toward the south (negative slice offsets) is primarily approaching us and seen at lower velocities relative to the disk emission. Similarly, outflow emission toward the north is primarily at velocities higher than the disk emission. Consequently, emission in pV slices shifts from lower to higher velocities relative to the disk model when the offset from the major axis increases (see Figure 12 in Appendix C). We designed the disk mask to be wide enough to capture the disk emission but exclude the asymmetric component caused by outflows.

We define a "nondisk" mask that is the mathematical complement of the disk mask, with the addition of removing emission from known sources (portions of the spiral arms) that were not included in our model of the central disk and are not of interest for this analysis.

3.6. Identifying Outflows in the Nondisk Component

We identify three different types of structures in the nondisk component (Figure 6; contours in Figure 7 highlight these structures):

Figure 6.
Standard image High-resolution image
Figure 6.

Figure 6. Comparison between the original moment maps and separated disk/nondisk components. (The outline of the maps is defined by the observed field of view and the square region considered for separating the kinematic components.) (a) Moment 0 (integrated intensity) of the original image (top), disk component (middle), and nondisk component (bottom). The logarithmic color scales are identical for all panels and chosen to also show the fainter nondisk component which saturates the inner regions of the disk. Contours are drawn at $\mathrm{log}\left(F\ [{\rm{K}}\,\mathrm{km}\,{{\rm{s}}}^{-1}]\right)=1.7,2.0,2.3,2.6,2.9,3.2,3.5;$ for clarity, only every other contour is drawn for CO(3–2). (b) Moment 1 (intensity-weighted velocity) of the original image (top), disk component (middle), and nondisk component (bottom). Contours are drawn at 150, 200, ..., 350 km s−1. The noise edge visible in CO(3–2) is due to the primary beam correction required to derive accurate fluxes.

Standard image High-resolution image
Figure 7.

Figure 7. A zoom-in on the nondisk component of CO(3–2) (the bottom left panels in Figures 6(a) and (b)). Top: moment 0 (integrated intensity) with contours at $\mathrm{log}\left(F\ [\mathrm{km}\,{{\rm{s}}}^{-1}]\right)=2.0,2.5,3.0$. Bottom: moment 1 (intensity-weighted velocity). The thick contours show the regions discussed in the text (Section 4.3): gas that is kinematically not consistent with disk rotation but cospatial with the disk in projection, and the western superbubble to the northwest of the disk.

Standard image High-resolution image

(1) Emission that is colocated with the central disk and bar in projection. This is visible as a ridge in CO(3–2) (inner contour in Figure 7) and also present but less apparent in CO(1–0) and CO(2–1). The structure is unlikely to be an outflow. It appears more likely to be an additional kinematic component of the disk/bar that is not included in the model we used for the separation. We therefore do not consider this gas to contribute to the total mass outflow rate.

(2) Emission associated with the so-called western superbubble, located to the west and north of the central starburst region (Sakamoto et al. 2006; Bolatto et al. 2013; shown by the western contour in Figure 7). This feature is already known to be kinematically distinct from the surrounding gas. Part of it is likely the base of the northern outflow cone (and giving rise to the NW streamers identified by Bolatto et al., for example), but it is difficult to know what portion of the emission should be associated with a net outflow. In our calculations below, we exclude this feature from the total outflow rate of NGC 253, although it likely has some contribution to the outflow.

(3) The remaining gas associated with the nondisk component is organized in small clumps along the edge of the disk region or beyond it. Some of this gas is not discernible as individual structures, particularly in the CO(1–0) and CO(2–1) cubes, perhaps due to the resolution but maybe also due to the excitation conditions, constituting extended regions with diffuse emission. Some of the emission is located in well-defined structures known to be part of the outflow, such as the SW streamer, which is apparent in all CO transitions.

In summary, the nondisk component consists of these three subcomponents: structures that we associate with a net "outflow," structures that are part of the "western superbubble," and structures that are colocated with the "disk." The latter is not associated with the outflow, while parts of the western superbubble may contribute to it. Below, we calculate properties for the two components, disk and nondisk, and its subcomponents individually where it is feasible to do so.

4. Results

The process described in the previous section allows us to estimate the properties of the galactic outflow and other structures. A 2D representation of the separated data cubes is shown in Figure 6 in the form of moment maps for integrated intensity (moment 0) and intensity-weighted velocity (moment 1) for all three CO transitions. Striping artifacts due to the pV cuts used in the separation method are present in the disk and nondisk components, visible as straight lines parallel to the major axis. This is primarily aesthetic. We tested their effects on the fluxes and derived velocities by varying the slice width and found them to be negligible.

4.1. CO Luminosities

We quantify in Table 2 the CO luminosities of the disk and nondisk components. We measure luminosities of 2.8 × 108 K km s−1 pc2, 2.3 × 108 K km s−1 pc2, and 1.8 ×108 K km s−1 pc2 for CO(1–0), (2–1), and (3–2), respectively, in the central disk of NGC 253. The nondisk component is, naturally, much fainter with luminosities of ∼4.2 × 107 K km s−1 pc2 for CO(1–0), ∼4.2 × 107 K km s−1 pc2 for (2–1), and ∼4.2 ×107 K km s−1 pc2 (3–2). These correspond to approximately 12.9%, 16.4%, and 6.5% of the total luminosity. These luminosities are measured over the sliced area (see Figure 4) for which the coverage is not the same among the data sets. We therefore also measure luminosities integrated over the same spatial region, here defined as the overlap between the data sets. This overlap amounts to 885 arcsec2 (2.55 × 105 pc2). The luminosities in the overlap area are disk: 2.6 × 108 K km s−1 pc2, 2.1 ×108 K km s−1 pc2, and 1.8 × 108 K km s−1 pc2; nondisk: 2.6 ×107 K km s−1 pc2, 2.4 × 107 K km s−1 pc2, and 1.2 × 107 K km s−1 pc2 for CO(1–0), (2–1), and (3–2), respectively.

Table 2.  Results of Separating Disk from Nondisk Emission in NGC 253

Quantity Units CO(1–0) CO(2–1) CO(3–2)
    Disk Nondisk Disk Nondisk Disk Nondisk
Luminosity
LCO K km s−1 pc2 2.8 × 108 4.2 × 107 2.3 × 108 4.5 × 107 1.8 × 108 1.2 × 107
Fraction % 87 13 84 16 94 6.5
Molecular Gas Mass Mmola
Totalb M 3.1 × 108 4.5 × 107 3.1 × 108 6.1 × 107 2.9 × 108 2.0 × 107
Outflowc M   2.7 × 107   4.1 × 107   8.3 × 106
Superbubbled M   8.9 × 106   8.9 × 106   5.8 × 106
Other-diske M   7.6 × 106   7.4 × 106   5.8 × 106
Molecular Mass Outflow Rate $\dot{M}$ f
Outflow (continuous)g M yr−1   14   20   2.7
Outflow (constant)h M yr−1   29   39   4.8
Kinetic Energy Ekini
Outflow (continuous)g erg s−1   3.9 × 1054   4.5 × 1054   6.5 × 1053
Outflow (constant)h erg s−1   2.5 × 1054   3.1 × 1054   4.3 × 1053
Momentum Pj
Outflow (continuous)g M km s−1   6.9 × 108   8.7 × 108   1.2 × 108
Outflow (constant)h M km s−1   4.8 × 108   6.4 × 108   8.0 × 107

Notes. Uncertainties for these quantities are discussed in the corresponding subsections of Section 4. Sources of error are discussed and quantified in the respective subsections of Section 4.

aMolecular gas mass derived using a conversion factor for CO(1–0) emission of ${X}_{\mathrm{CO}}=0.5\times {10}^{20}{\left({\rm{K}}\mathrm{km}{{\rm{s}}}^{-1}\right)}^{-1}$, including the contribution of helium, and assuming CO brightness temperature line ratios of r21 = 0.80 and r31 = 0.67 for CO(2–1) and CO(3–2) relative to CO(1–0). bCO line luminosity of all emission considered consistent with disk rotation (disk) and not consistent with disk rotation (nondisk), respectively. cNondisk excluding the western superbubble and the gas that is cospatial with the projected disk. dNondisk emission belonging to the western superbubble as defined by Sakamoto et al. (2006). eNondisk gas that is cospatial with the disk in projection. See Section 4.3 for the definition. fDeprojected molecular mass outflow rate. Fiftieth percentile best estimate assuming a flat distribution of outflow inclinations for the unknown geometry. gOutflowing gas as defined by note (c) under the assumption of continuous mass ejection without accelerations to the gas after ejection. hOutflowing gas as defined by note (c) under the assumption of approximately constant starting mass outflow rate over the lifetime of the starburst. iDeprojected kinetic energy of the molecular gas. Fiftieth percentile best estimate assuming a flat distribution of outflow inclinations for the unknown geometry. jDeprojected momentum of the molecular gas. 50th percentile best estimate assuming a flat distribution of outflow inclinations for the unknown geometry.

Download table as:  ASCIITypeset image

An interesting result coming out of our decomposition is that not all of the material we identify as "outflow" is in well-defined structures such as the streamers identified by Bolatto et al. (2013). Correctly estimating the outflow rate requires also accounting for a diffuse extended component.

It is important to compare our fluxes to measurements in the literature. Mauersberger et al. (1996) found a CO(2–1) luminosity of 1.2 × 106 K km s−1 arcsec2, which translates13 to 3.5 × 108 K km s−1 pc2 or 1.3 times our measurement. Their observations cover 80'' × 60'', an area similar to our CO(1–0) observations (but ∼4 times larger than the area of our CO(3–2) observations). For the outflow CO(1–0) luminosity, Bolatto et al. (2013) derived an estimate of 2.0 × 107 K km s−1 pc2 by summing over individual identified molecular outflow features. This includes flux from the "superbubble" component, so it is probably better compared to the sum of our "outflow" and "superbubble" components of ∼3.6 × 107 K km s−1 pc2. Given the large methodological differences and the importance of the diffuse emission, these numbers are in reasonable agreement.

4.2. Masses of Components

The total gas mass M is estimated from the CO line luminosity, using the conversion factor ${X}_{\mathrm{CO}}=0.5\times {10}^{20}\ {\left({\rm{K}}\mathrm{km}{{\rm{s}}}^{-1}\right)}^{-1}$ cm−2 corresponding to ${\alpha }_{\mathrm{CO}}=1.1\,{M}_{\odot }{\left({\rm{K}}\mathrm{km}{{\rm{s}}}^{-1}{\mathrm{pc}}^{-1}\right)}^{-1}$ discussed by Leroy et al. (2015a) for the central starburst region. This value accounts for the effects of moderate optical depth, high-velocity dispersion, and warm gas temperatures that are likely to dominate the central regions of NGC 253. The masses we report include the contribution of helium to the total mass. To compute masses using the CO(2–1) and CO(3–2) transitions, we assume typical line ratios of r21 = 0.80 and r31 = 0.67 relative to CO(1–0) as implied by Zschaechner et al. (2018). Note that we do not measure line ratios from the images but adopt a uniform factor to keep the mass measurements from the three observed CO lines independent.

Table 2 lists the masses corresponding to the disk and the nondisk components. Uncertainty in the mass estimates arises primarily from the assumed conversion factor and the apportioning of emission among the different components. The calibration uncertainty for the flux measurements is ∼10%–15% for the ALMA observations. Overall, we adopt a systematic error of factor ∼2 for the the derived masses.

The molecular masses derived from the three CO transitions are very similar. They match within 10% for the disk component, and within 50% for the nondisk component. We estimate the total gas mass in the center of NGC 253 to be ∼3.5 × 108 M (adding the disk and nondisk components), with estimates in the range of 3.1–3.6 × 108 M for the different transitions. About 85% of the total mass is in the disk component. The masses estimated in the nondisk components using CO(1–0) and CO(2–1) are fairly similar at 4.5 × 107 M and 6.1 × 107 M, whereas in CO(3–2) we detect a lower mass, 2.0 × 107 M, a consequence of the lower luminosity. The nondisk masses are primarily contributed by the outflow component (∼50%). About 20%–30% of mass is in the western superbubble and 12%–30% is cospatial with the disk but kinematically distinct.

It is important to compare these mass estimates to previous results for the total molecular gas mass in NGC 253, noting that our analysis covers the central 45'' × 25'' (750 pc × 400 pc). Toward the east, ∼10% of the known molecular gas close to the center is not covered by our CO(3–2) observations and thus not considered in this analysis. The agreement with previous measurements is very good. Mauersberger et al. (1996) reported a mass of 1.3 × 108 M over a similar area (80'' × 60'' in the center of NGC 253), but this was based on a different distance and XCO. After correcting for those differences, their luminosity corresponds to 4.2 × 108 M, consistent with our measurement. Using the same distance and the same 1–0 observations, Leroy et al. (2015a) measured a molecular mass of 3.5 × 108 M. Pérez-Beaupuits et al. (2018) reported a total gas mass of 4.5 × 108 M derived from the submillimeter dust spectral energy distribution, which is very consistent with our result given the very different methodologies.

No estimates in the literature separate the "disk" and "nondisk" components as we do above. Previous estimates of the outflowing mass range from a lower limit of 6.6 × 106 M calculated for the optically thin limit (Bolatto et al. 2013), to 2–4 × 107 M, when accounting for optical depth (Zschaechner et al. 2018). Because we identify an outflowing mass of ∼5 × 107 M, the agreement with the latter estimate is fairly good. Note, however, that these studies derive the outflowing mass from individual features rather than using the pV information as we do here in a systematic way.

4.3. Mass Outflow Rate

Mass flow rate is defined as the flux of mass per unit time through a surface. In our case, we are interested in the flow of molecular gas mass through a virtual closed surface around the center of NGC 253 at a given distance. Note that an individual outflow feature observed over a certain length, such as the SW streamer, can develop in at least two ways: as the distance of an outflow from its origin corresponds to time since ejection times velocity, continuously outflowing gas results in extended streaming structures. Gas ejected at a single ejection event in the past with a distribution of ejection velocities, on the other hand, will also result in an extended streamer. In reality, gas will be ejected with a distribution of velocities at a varying rate over a period of time, and in order to interpret the measurements, we need to make some simplifying assumptions. We chose two edge cases to span the range of different interpretations: (1) the gas does not experience accelerations after being launched (however, see Walter et al. 2017), and (2) that the gas outflow rate is approximately constant with time. For all calculations, however, we assume that the projected direction of flow is perpendicular to the central plane of the bar and that CO emission traces the mass with a constant conversion factor.

We compute the outflow rate both as a function of distance and as a function of time. If we assume that the mass outflow rate has been approximately constant over the lifetime of the starburst, for example, a diminishing outflow rate as a function of distance would suggest that gas is either launched with or somehow develops a distribution of velocities. Conversely, if we assume that the present-day velocity has been constant since the gas was ejected, we can derive a history of the mass outflow rate as a function of time and account for a variable mass outflow rate. Both interpretations are equally, but not simultaneously, valid.

For the detailed calculation of the mass outflow rate, we proceed as follows. The mass outflow rate is $\dot{M}=M\,{t}^{-1}$ with mass M and relevant timescale t. For each image element i (3D pixel or sometimes also called voxel), we calculate the outflow rate ${\dot{m}}_{i}$ of the gas that was ejected at time ${t}_{\mathrm{eject},i}$ over the time interval ${\rm{\Delta }}{t}_{\mathrm{cross},i}$, as the ratio of mass of the pixel mi to the pixel-crossing interval tcross,i. The ejection time and pixel-crossing interval are functions of the outflow velocity vi and the distance si between the current pixel position and the launching site, and the pixel size in the direction of the flow Δs, respectively. We therefore compute

Equation (2)

Equation (3)

Equation (4)

obtaining a mass outflow rate ${\dot{m}}_{i}$, a distance si, and an ejection time teject,i for each pixel in the "outflow" component. Note that this approach takes the 3D phase space information into account by treating pixels independently. Typically, a sight line shows multiple pixels with emission at different velocities that all contribute an outflow rate with their respective mass, distance, and velocity. We then bin the outflow rates ${\dot{m}}_{i}$ by ejection time ${t}_{\mathrm{eject},i}$ and integrate over the time range $\left[{T}_{1},{T}_{2}\right]$ to obtain the average outflow rate in this time interval,

Equation (5)

Similarly, binning by distance results in the average outflow rate at a given distance,

Equation (6)

Performing binning on a sequence of time intervals yields the outflow rate history, while binning in distance tells us how far from the launching site a given fraction of the mass is able to escape.

Calculating velocity v and distance s requires knowledge about the geometry and origin of each outflowing gas parcel. The simplest assumption, used here, is that on average, outflows are launched in the plane of the central region of the galaxy, which corresponds to launching on the major axis. The distance s is thus the projected distance to the major axis on the edge of an outflow cone with a given opening angle. Note that the outflow originates from an extended region in the disk and the term cone thus refers to a cutoff cone (called a frustum in geometry). The velocity v is the velocity difference between the launching site and current velocity of the outflow parcel, i.e., the velocity difference over the distance s. The velocities of both the launching site and the projected distance are uncertain. The velocity changes by ±25 km s−1 when an outflow originates from the northern/southern edge of the observed CO disk (above/below the plane), while the projected distance traveled by the gas changes by ±1farcs25 (±20 pc).

Distance s, ejection timescale teject, and pixel-crossing timescale tcross are measured as projected quantities that need to be deprojected to account for the outflow geometry. The bright molecular streamers (the SW and SE streamers) seem to lie at the edge of the ionized outflow cone with a ∼60° opening angle (Bolatto et al. 2013). Assuming that all molecular outflows are along this cone and that the axis of the cone is oriented perpendicular to the disk (i = 78°), the range of the effective inclination of outflowing gas can be anywhere between θ = 48° and θ = 108°. Deprojected velocity, ${v}_{\mathrm{depro}}\,={v}_{\mathrm{obs}}/\sin \theta $, and distance, ${s}_{\mathrm{depro}}={s}_{\mathrm{obs}}/\cos \theta $, have a direct effect on the deprojected outflow rate, ${\dot{m}}_{\mathrm{depro}}={\dot{m}}_{\mathrm{obs}}\tan \theta $, and also on the inferred time and distance evolution of the outflow rate. We use a Monte Carlo approach to derive the errors introduced by deprojection, assuming that the outflow direction has an equal probability of being in any direction along the surface of the outflow cone.

Figure 8 shows the molecular mass outflow rate as a function of time or distance, corresponding to the two alternative interpretations we discuss above: a flow where the distribution of material is interpreted as resulting from the history of the mass outflow rate (top panel) and one where we show the mass outflow rate as a function of distance, which under the assumption of a constant outflow rate over the last several megayears can be interpreted as the efficiency of ejection to a given distance (bottom panel). Indeed, for an outflow with a distribution of velocities, the slower material will not travel as far in a given time, and neither will it escape the galaxy if it does not have a high-enough velocity. Close to the starburst region (or at small times since ejection), the mass outflow rate drops to zero, because it becomes increasingly difficult to separate the "outflow" component from the "disk" component. At large values of distance or time, it also drops to zero, due to a decreasing amount of outflowing molecular material detected far from the starbursts (and the fact that the observations have a limited field of view). The constant outflow rate out to ∼300 pc is in tension with Kim & Ostriker (2018), who find a steeply dropping "cold" (T < 5050 K) component in their TIGRESS simulation. Within 400 pc, they find the average mass-loading factor to drop by two orders of magnitude. It is unlikely that the SFR in NGC 253 has increased by two orders of magnitude within the past 1–2 Gyr, which would alter the observed constant outflow rate profile to be consistent with the Kim & Ostriker (2018) simulation. Note, however, that their simulation recreates solar neighborhood-like conditions instead of a starburst. A direct comparison may thus not be possible.

Figure 8.

Figure 8. Deprojected molecular mass outflow rate averaged over 0.1 Myr as a function of time since ejection (top) and as a function of deprojected distance between outflow and launching site (bottom). The top panel implicitly assumes continuous mass ejection without accelerations to the gas after ejection, while the lower panel assumes an approximately constant starting mass outflow rate over the lifetime of the starburst. The shaded area indicates approximate errors (16th–84th percentile), which are dominated by uncertainties in the deprojection geometry. Dotted lines represent the ranges where confusion with gas in the disk occurs and where the limited field of view affects the completeness.

Standard image High-resolution image

Our data show that the average outflow rates within 20'' (340 pc) from the major axis are 29 M yr−1 (${}_{-0.35}^{+0.48}$ dex), 39 M yr−1 (${}_{-0.34}^{+0.49}$ dex), and 4.8 M yr−1 (${}_{-0.39}^{+0.50}$ dex) for CO(1–0), (2–1), and (3–2), respectively. Similarly, within the past 1.0 Myr, the average outflow rates are 14 M yr−1 (${}_{-0.29}^{+0.25}$ dex), 20 M yr−1 (${}_{-0.37}^{+0.27}$ dex), and 2.7 M yr−1 (${}_{-0.56}^{+0.22}$ dex) for CO(1–0), (2–1), and (3–2), respectively. The uncertainties, indicated by the 16th–84th percentiles in the Monte Carlo described above, are substantial at a factor of 2–3. Real systematic uncertainties are even larger, because there can be conversion of molecular into atomic material (see Leroy et al. 2015b), or in general variations in the CO-to-H2 conversion.

Note that the average outflow rates quoted above differ between the two representations, with the median outflow rate as a function of distance being about twice as high as a function of time. The outflowing mass is identical in both cases, and the difference arises solely from binning. Comparing between lines, it is apparent that as measured in CO(3–2), the outflow rate is roughly one order of magnitude lower than for the lower two transitions. This is a direct consequence of the lower mass detected in CO(3–2) and the smaller field of view of those observations. The CO(3–2) observations cover only ∼12farcs5 (∼210 pc projected) above/below the disk and thus miss significant amounts of nondisk gas. Their lower surface brightness sensitivity means we also fail to detect a diffuse nondisk component, as we see in the two lower lines. The measurements in CO(3–2) should thus be interpreted as a lower limit, and in that sense they are consistent with those for the lower two transitions.

Overall, the deprojected total mass outflow rate in the starburst of NGC 253 is most likely in the range ∼14–39 M yr−1 as derived from CO(1–0) and CO(2–1) with ∼0.4 dex uncertainty. The large spread arises due to different interpretations of the kinematics of the observed gas while the errors are due to unknown geometry. The majority of this outflow rate is contributed by massive outflows alongside the disk like the SW/SE streamers, with a significant contribution by diffuse molecular gas.

The present-day SFR in the central region of NGC 253 is 1.7–2.8 M yr−1, derived from radio continuum and far-infrared measurements (Ott et al. 2005; Bendo et al. 2015; Leroy et al. 2015a). This results in a mass-loading factor $\eta ={\dot{M}}_{\mathrm{out}}/{\dot{M}}_{\mathrm{SFR}}$ in the range η ∼ 5.4–23.5. Note that this is for gas ejected as far as 340 pc. We do not currently know what fraction of the gas makes it to the far regions of the halo or reaches escape velocity from the system. Theoretical works suggest that most of the molecular outflow will not escape but rain back down on the galaxy (e.g., Shapiro & Field 1976 up to recent work by Kim & Ostriker 2018 or Tollet et al. 2019). In our data, no gas reaches the escape velocity of vesc = 500 km s−1 (Walter et al. 2017). The uncertainty on vesc is substantial, so allowing a factor of 2 is still plausible. At vesc = 250 km s−1, the fraction of gas above vesc by mass is 0.5%, 0.5%, and 6.0% for CO(1–0), CO(2–1), and CO(3–2), respectively. The mismatch between the lower transitions and CO(3–2) implies that some high-velocity gas can be found on small scales that is blurred out in the low-resolution observations.

This estimate of the molecular mass outflow rate is higher than the lower limit found by Bolatto et al. (2013) for optically thin emission. Zschaechner et al.'s (2018) analysis of the CO line ratios in the SW streamer shows that the emission there is optically thick, which the authors used to rescale the Bolatto et al. (2013) measurements, finding a NGC 253 galactic outflow rate of 25–50 M yr−1. The result presented here, a mass outflow rate of ∼14–39 M yr−1, is consistent with this number using an independent and a more complete methodology than the original work.

From Hα observations by Westmoquette et al. (2011), we can estimate the ionized outflow rate to be ∼4 M yr−1 using their ionized mass (M = 107 M) and typical velocity (200 km s−1) at a mean deprojected distance (510 pc). X-ray observations yield comparable values. Strickland et al. (2000) found an upper limit of 2.2 M yr−1 assuming a standard outflow velocity of 3000 km s−1. The upper limit reported in Strickland et al. (2002) translates to 2.3 M yr−1 when assuming 3000 km s−1 outflow velocity and a reasonable 10% filling factor. These estimates scale linearly with the unknown velocity and also depend on the unknown metallicity and filling factor in the outflow. Estimates of the outflow rate in neutral gas are not known in the literature but are arguably at a similar level. The molecular phase thus clearly dominates the mass budget in the outflow close to the disk as found in other galaxies (e.g., M82, Leroy et al. 2015b; and simulations, e.g., Kim & Ostriker 2018).

4.4. Outflow Energy and Momentum

Similar to the mass outflow rate, energy and momentum can be calculated as a function of time and distance, which is shown in Figure 9. In Equations (5) and (6), the molecular outflow rate ${\dot{m}}_{i}$ is replaced by kinetic energy ${E}_{\mathrm{kin},i}=\tfrac{1}{2}{m}_{i}\,{v}_{i}^{2}$ or momentum ${P}_{i}={m}_{i}\,{v}_{i}$. As with the outflow rate, the dominant sources of error are the uncertainty in the launching site and the geometry for which we Monte Carlo the errors as described before. Our median estimate with 16th and 84th percentile uncertainties are given below and in Table 2.

Figure 9.

Figure 9. Deprojected kinetic energy (left) and deprojected momentum (right) of the molecular outflow averaged over 0.1 Myr as a function of time since ejection (top) and as a function of deprojected distance between the outflow and launching site (bottom). The top panel implicitly assumes continuous mass ejection without accelerations to the gas after ejection, while the lower panel assumes an approximately constant starting mass outflow rate over the lifetime of the starburst. The shaded area indicates approximate errors (16th–84th percentile), which are dominated by uncertainties in the deprojection geometry. Dotted lines represent the ranges where confusion with gas in the disk occurs and where the limited field of view affects the completeness.

Standard image High-resolution image

The kinetic energy in the outflow integrated over the past 1.0 Myr is 3.9 × 1054 erg (${}_{-0.75}^{+0.91}$ dex) in CO(1–0), 4.5 × 1054 erg (${}_{-0.80}^{+0.94}$ dex) in CO(2–1), and 6.5 × 1053 erg (${}_{-0.83}^{+0.58}$ dex) for CO(3–2). Within 20'' (340 pc), the kinetic energies amount to 2.5 × 1054 erg (${}_{-0.65}^{+0.96}$ dex) in CO(1–0), 3.1 × 1054 erg (${}_{-0.65}^{+0.96}$ dex) in CO(2–1), and 4.3 × 1053 erg (${}_{-0.64}^{+0.98}$ dex) for CO(3–2). For the reasons described above, the CO(3–2) measurement is a lower limit, thus the results for the lower transitions are consistent.

NGC 253 does not appear to host an energetically important AGN, and the outflow is driven by the starburst. It is interesting then to compare our results for the kinetic energy to the energy released by the starburst. We assume the current SFR of ∼2.8 M yr−1 in the central region (Ott et al. 2005; Bendo et al. 2015), which has been approximately constant over the last few megayears.

The total energy Ebol produced by the starburst is simply the time-integrated bolometric luminosity Lbol, which depends14 on the bolometric magnitude Mbol:

Equation (7)

Equation (8)

According to Starburst99 (Figure 46 in Leitherer et al. 1999), the bolometric magnitude of a starburst at an age of 107–108 yr is Mbol ∼ −20.5 for SFR = 1 M yr−1. The total energy output of the starburst over the past 1 Myr is thus 4.2 × 1057 erg. The observed kinetic energy ∼3.9–4.5 × 1054 erg in the outflow is a factor of ∼103 lower, which places the coupling efficiency of the outflow kinetic energy to starburst energy at ∼0.1%.

In terms of only kinetic energy, the fraction is higher. It is primarily supernovae and winds that supply kinetic energy to the ISM, which can be estimated from the energy deposition rate according to Leitherer et al. (1999) as given in Chisholm et al. (2017) and Murray et al. (2005):

Equation (9)

Each SN releases approximately 1051 erg in kinetic energy, with the progenitor releasing a similar amount of kinetic energy by winds during its lifetime (e.g., Leitherer et al. 1999). The approximate total kinetic energy released by SNe in the past 1 Myr is then ∼5.3 × 1055 erg, compared to the ∼3.9–4.5 ×1054 erg we observe in the outflow. Hence, the observed starburst is sufficient to kinetically power the measured molecular outflows with ∼8% efficiency.

The commonly adopted 50% relative contribution of wind feedback is a first-order estimate that is subject to environmental dependence and requires careful modeling to determine precisely (e.g., Leitherer et al. 1999). Furthermore, it should be noted that the observed outflow energy and its error are based on a fixed mass conversion factor that may vary. The uncertainty on the energy coupling efficiency is thus substantial, and it should be understood as an order-of-magnitude comparison.

The above calculation ignores the contribution of other energies, such as the turbulent energy within the molecular outflow and the kinetic energy of the neutral and ionized gases. Matsubayashi et al. (2009) derived a kinetic energy of the ionized wind in NGC 253 of 1.3 × 1053 erg or more than one order of magnitude lower than the molecular outflow kinetic energy. The molecular outflow is slower (50–100 km s−1 on the scales we observed here) than the ionized outflow (up to ∼400 km s−1; Matsubayashi et al. 2009) but also more massive. The ionized outflow thus has only a very small effect on the total kinetic energy and the coupling efficiency.

Deprojected outflow momenta integrated over the past 1.0 Myr are 6.9 × 108 M km s−1 (${}_{-0.49}^{+0.50}$ dex), 8.7 ×108 M km s−1 (${}_{-0.57}^{+0.57}$ dex), and 1.2 × 108 M km s−1 (${}_{-0.59}^{+0.33}$ dex) for CO(1–0), (2–1), and (3–2), respectively. Within 20'' (340 pc) deprojected distance from the launching site, the outflow momenta integrate to 4.8 × 108 M km s−1 (${}_{-0.35}^{+0.48}$ dex) in CO(1–0), 6.4 × 108 M km s−1 (${}_{-0.34}^{+0.49}$ dex) in CO(2–1), and 8.0 × 107 M km s−1 (${}_{-0.39}^{+0.50}$ dex) in CO(3–2).

The momentum released initially by SNe is given in Murray et al. (2005):

Equation (10)

Equation (11)

In 1 Myr, a constant SFR of 2.8 M yr−1 yields 8.9 ×108 M km s−1. Assuming a contribution by stellar winds of the same order (Leitherer et al. 1999), the total momentum is 1.8 × 109 M km s−1, or roughly twice the observed outflow momentum. SNe, however, gain significant amounts15 of momentum by sweeping up surrounding material. From simulations, the total momentum supplied to the ISM is expected to be 2.8 × 105 M km s−1 per SNe (Kim & Ostriker 2015 and references therein). For a constant SFR of 2.8 M yr−1 over 1 Myr, this amounts to 1.0 × 1010 M km s−1 or 2.0 × 1010 M km s−1 when adopting 50% contribution by stellar winds, which is about four times the observed momentum. The efficiency of transferring feedback momentum to outflow momentum is thus in the range of 27%–49%, considering the initially available momentum, or a 2.5%–4% efficiency for total to outflow momentum transfer.

These outflow momenta are much higher than the momentum currently produced by young (<10 Myr) super star clusters in the starburst. Leroy et al. (2018) list 14 candidate clusters that together produce 1.5 × 107 M km s−1 measured from gas kinematics, a factor 10–100 lower than the observed outflow momentum. The currently forming (super) star cluster thus could not have launched the outflow but the feedback of another population of stars is needed to explain the observed outflows. This is indicative of the time delay of SF feedback.

Energy and momentum curves in Figure 9 differ only by a factor v but follow a similar evolution. This implies that the median velocity at a given distance must be roughly constant along the outflow. As the curves as a function of distance are roughly constant within 50 pc < s < 300 pc, especially for kinetic energy, the outflow mass at a given distance must also be approximately constant along the outflow. The decline in energy and momentum below 50 pc is caused by a decrease in outflow mass, again because both curves follow a similar trend. This is at least partially related to the difficulty of separating the outflow from the disk, where the former emerges from the latter. The decrease could also be interpreted physically as the outflow sweeping up mass while emerging from the disk. An estimation of the relative importance of these effects requires high-resolution modeling of the outflow that are not possible yet because we do not know the detailed outflow geometry. The drop beyond ∼300 pc (∼200 pc in CO(3–2)) is partially related to reaching the edge of the field of view. Discerning this effect from an actual decrease is not possible with our data as we do not know the inclination at every location in the outflow. The edge of the field of view thus corresponds to a range of deprojected distances from the disk, which gradually depresses the curve rather than showing a sudden drop. A physical reason for the decrease could be the destruction of the molecular gas, e.g., photodissociation by the intense starburst radiation or ionization.

The kinetic energy and momentum evolution in Figure 9 thus suggest both energy and momentum conservation along the outflow from ∼50 pc to ∼300 pc, as well as approximately constant molecular gas mass.

When additionally assuming no acceleration of the outflow after launch, it becomes possible to study the time evolution. The corresponding plots (Figure 8 top and 9 top) all show a peak within the past 0.5 Myr and steady decrease toward earlier gas ejection times. Corresponding to the decline toward zero distance, the decrease toward zero ejection time is most likely a methodological complication. From the peak at teject = 0. 2–0.3 Myr, kinetic energy and momentum in the outflow drop by a factor of 10 within ∼2 Myr. This decline would be physically plausible if the starburst in NGC 253 is very young and takes into account a time delay between the start of star formation, feedback, and efficient outflow driving (superbubble breakout). For the observed age of the starburst of 20–30 Myr (Rieke et al. 1980; Engelbracht et al. 1998) this scenario is implausible. Time delays of >20 Myr are longer than the lifetime of the most massive stars. A younger generation of massive stars at an age of ∼6 Myr (Kornei & McCrady 2009) may, however, drive the currently visible molecular outflows. If this were to be true, a time delay between star formation and outflow launching of ∼4 Myr is implied. Outflow launching in this context means the time after which the outflow reaches a mass loading η > 1. The time delay is 2 Myr until the outflow carries more energy (momentum) than the feedback kinetic energy (momentum) of a single high-mass star. Note that these rough estimates depend on the assumption of no acceleration (neither positive nor negative) of the outflow after being launched from the disk, which might be a close enough approximation on these scales of a few hundred parsecs. The very young (≲1 Myr) and still deeply embedded super star cluster discussed recently by Ando et al. (2017) and Leroy et al. (2018) are most likely too young to have affected the observed molecular outflow.

5. Summary and Conclusions

We present CO(3–2) observations taken with ALMA that offer an unprecedented resolution of ∼0farcs15 (∼2 pc) in the starbursting center of NGC 253. The new high-resolution data show structures consistent with previous lower resolution observations in other CO lines, revealing the complexity of the molecular ISM in a starburst on scales of a few parsecs.

We use archival CO(1–0), CO(2–1), and the new CO(3–2) ALMA observations to perform a ppV decomposition of the emission into different structures. The bulk of the emission is associated with a rotating disk with streaming motions due to the bar. The rest of the emission is incompatible with a simple kinematic model of a disk plus a bar. This "nondisk" component is further decomposed into an outflow, an expanding superbubble (part of which may be associated with outflowing gas), and a potential second kinematic component within the disk.

We find CO line luminosities of the disk component of 2.8 × 108 K km s−1 pc2, 2.3 × 108 K km s−1 pc2, and 1.8 ×108 K km s−1 pc2 for CO(1–0), (2–1), and (3–2), respectively. The fractional luminosity of the nondisk component is small, amounting to ∼7%–16% of the total. A significant amount of the outflow emission we identify is faint and diffuse, while part of the emission is in discrete, higher surface brightness structures (e.g., the SW streamer).

Assuming a starburst conversion factor, we estimate the molecular gas mass from the three CO transitions. Masses match within 10% for the disk component and within 50% for the nondisk component. The total gas mass in the center of NGC 253 is ∼3.6 × 108 M, with ∼0.5 × 108 M in the nondisk component.

We further estimate the deprojected molecular mass outflow rate, kinetic energy, and momentum in the starburst of NGC 253. The observed gas distribution can be interpreted to have formed in two ways: (1) by a constant starting mass outflow rate over the lifetime of the starburst and (2) through continuous gas ejection without acceleration of the gas after ejection. In the first interpretation, the molecular mass outflow rate averaged over a deprojected distance of 340 pc (20'') from the launching site is 29–39 M yr−1. Typical uncertainties are 0.4 dex. The majority of this outflow rate is contributed by massive localized features such as the SW/SE streamers, with a significant contribution by diffuse molecular gas. The mass-loading factor $\eta ={\dot{M}}_{\mathrm{SFR}}/{\dot{M}}_{\mathrm{out}}\sim 14\mbox{--}20$ is relatively high. Due to the limited field of view of our observations, this η applies to gas ejected as far away as 340 pc: the fraction of mass that makes it to the far regions of the halo or escapes is not known. The kinetic energy of the molecular outflow within 340 pc from the launching site is 2.5–3.1 × 1054 erg with a ∼0.8 dex error. The coupling efficiency of kinetic energy in the outflow to the total energy released by the starburst is ∼0.1% while the coupling to only the kinetic energy is higher at ∼8%. Including other phases of the outflow would increase this efficiency. The kinetic energy of the ionized outflow is negligible relative to the molecular outflow. The outflow momenta within the same distance are 4.8–6.4 × 108 M km s−1 (error ∼0.5 dex) which is ∼2.5%–4% of the momentum supplied by SNe and winds. These best estimates for the physical properties of the outflow are derived from the CO(1–0) and (2–1) observations. The very high resolution of the CO(3–2) data is necessary to identify the outflow features that connect to the central regions.

When interpreting the outflow as a structure of constant velocity along the outflow, the time evolution can be reconstructed. We derive the outflow rate, kinetic energy, and momentum within the approximate dynamical timescale of 1 Myr and find lower values compared to the previous interpretation. The difference is systematic at the ∼30%–40% level. The outflow rate is 14–20 M yr−1 (0.3 dex), kinetic energy 2.5–3.1 × 1054 erg (0.8 dex), and momentum 4.8–6.4 × 108 M km s−1 (0.5 dex).

For all measurements given above, we assume a fixed starburst mass conversion factor of ${X}_{\mathrm{CO}}=0.5\times {10}^{20}{\left({\rm{K}}\mathrm{km}{{\rm{s}}}^{-1}\right)}^{-1}$. The quoted uncertainties are primarily systematic, due to the unknown geometry of the outflow and its launching sites. A further uncertainty of 30%–40% (∼0.1 dex) comes from the assumptions regarding the outflowing material (constant starting mass over the lifetime of the starburst versus continuous gas ejection without acceleration). These limitations need to be addressed in the future. In principle, ALMA can also provide the very high resolution and sensitivity needed to enable this detailed view of a starburst on larger scales than probed in this study.

The authors thank Jan-Torge Schindler and Roberto Decarli for insightful discussion and advice. This paper makes use of the following ALMA data: ADS/JAO.ALMA #2011.1.00172.S, #2012.1.00108.S, and #2015.1.00274.S. ALMA is a partnership of ESO (representing its member states), NSF (USA) and NINS (Japan), together with NRC (Canada), NSC and ASIAA (Taiwan), and KASI (Republic of Korea), in cooperation with the Republic of Chile. The Joint ALMA Observatory is operated by ESO, AUI/NRAO, and NAOJ. The National Radio Astronomy Observatory is a facility of the National Science Foundation operated under cooperative agreement by Associated Universities, Inc. Part of the work presented in this paper was carried out at the Finnish Center for Astronomy with ESO (FINCA).

The work of A.K.L. is partially supported by NASA ADAP grants NNX16AF48G and NNX17AF39G and the National Science Foundation under grants No. 1615105, 1615109, and 1653300.

Software: CASA (McMullin et al. 2007), astropy (Astropy Collaboration et al. 2013, 2018), APLpy (Robitaille & Bressert 2012).

Appendix A: Kinematic Model of the Central Molecular Gas

We derive a model for the velocity of the disk component from the CO(1–0) observations using the kinematic fitting tool diskfit (Spekkens & Sellwood 2007; Sellwood & Sánchez 2010; Sellwood & Spekkens 2015). As mentioned in Section 3.1, these models benefit from the large area, which is why we base them on the CO(1–0) observations. A 20σ threshold ensures that the model is fitted to the bright disk, excluding any fainter outflows.

In diskfit, we fit using the velocity field fitter. The names of the set options in diskfit are given in parentheses in the following. The model is fitted to all pixels within an ellipse of 75'' major axis length (regrad), PA = 53° (regpa), and ellipticity epsilon = 0.66 (regeps). Outside this range, we use a sampling factor of 2 pixels (istepout). During the fit, the center is held fixed while we fit for the disk position angle and ellipticity with initial guesses of PA = 53° and epsilon = 0.66 based on by-eye inspection (lines 9 and 10 of the parameter file). We allow the model to fit for nonaxisymmetric flows with a PA = 78° initial guess and order m = 2 (line 12), which means diskfit will fit for rotation plus a bisymmetric model with m = 2 perturbations to the potential (bar). As the CO(1–0) data cover the kinematic center, we set the inner interpolation toggle to true, which assumes the velocity raises linearly within the innermost fitted ring. We do not fit for radial flows (radial flows toggle) because it allows too many degrees of freedom and produces bad models, as warned in the diskfit manual. We further fit for the systemic velocity and exclude warps from the model. A model with these parameters is fitted in rings at radii 12farcs5, 25'', 37farcs5, 50'', 62farcs5, 75'', 87farcs5, 100'', 125'', 150'', 175'', 200'', 225'', 250'', 275'', and 300''.

The residuals show a slight mismatch in velocity of ∼20–30 km s−1 along the direction of the bar. This is likely due to the bar being underestimated because the CO(1–0) image covers only the inner half of the total extent of the bar. The mismatch gets larger when fitting a model to the smaller images of CO(2–1) and (3–2), which confirms that it is caused by the lack of observed area. We fit this mismatch in the velocity field with an additional 2D Gaussian component and add it to the velocity field of the diskfit model to obtain a better model. Note that this additional component is not physically motivated or meaningful but purely aims to counteract the effect of limited observation area.

Figure 10 shows the velocity field of the model in comparison to the input CO(1–0) velocity field. The model typically fits the observed velocity field better than ±25 km s−1; larger deviations occur mostly over small areas of order one beam size. The model thus successfully reproduces the large-scale velocity field.

Figure 10.

Figure 10. Input data and model represented as velocity fields. Top left: CO(1–0) velocity field to which the model is fitted, known foreground emission is removed; top right: model velocity field; bottom left: CO(1–0) velocity overlaid with model contours; bottom right: residual velocity. The velocity fields use the same color scale from 100 to 400 km s−1 with contours in steps of 50 km s−1 within that range. The residual velocity uses the same color scale relative to the systemic velocity of 250 km s−1 with contours from −50 to +50 km s−1 in steps of 25 km s−1.

Standard image High-resolution image

Appendix B: Velocity Width of the Disk Mask

The definition of disk mask is crucial for this analysis as it determines whether a molecular cloud is considered kinematically consistent with the disk or if it is potentially outflowing. The position of the disk mask in ppV space is set by the disk model, but the width (velocity range Δv) of the mask is a free parameter. From Figure 12, it is obvious that Δv depends on the distance from the major axis, which is most simply accounted for by a parameterization of the form ${\rm{\Delta }}v=a\exp \left(-{\left(\tfrac{x}{b}\right)}^{2}\right)+c$. Finding the best-fit values for a, b, and c is difficult to do mathematically as the fit would need to be on the disk component that we want to determine from the mask first. We therefore select values that visually fit the pV diagrams as best as possible. They are given in Equation (1).

Figure 11 shows five alternative masks that vary only in width by 10% from the best-fit mask. It is apparent that even slight changes of 10% deteriorate the fit between mask and disk emission. Narrower masks obviously do not cover all disk emission, whereas the wider masks include spike features that are kinematically inconsistent with disk rotation.

Figure 11.

Figure 11. Position–velocity diagrams for the central slice along the major axis (offset 0farcs0) overlaid with five different choices for the velocity width of the disk mask. Gray scale and overlays are identical to Figures 5 and 12. The central panel shows the visually best-fitting mask as defined by Equation (1). The other panels use masks of 80%, 90%, 110%, and 120% of the best-fit width. Even a 10% change in mask width leads to a noticeable mismatch in the high-resolution CO(3–2) data.

Standard image High-resolution image

The effect of a ${}_{-10}^{+10}$% (${}_{-0.04}^{+0.04}$ dex) variation in the mask velocity width results in a ${}_{-0.01}^{+0.01}$ dex change in the integrated disk luminosity for CO(1–0), CO(2–1), and CO(3–2). The nondisk components are less bright than the disk and thus shows a higher relative variation when changing the mask width: luminosities vary by ${}_{+0.08}^{-0.07}$ dex (${}_{+0.07}^{-0.06}$ dex, ${}_{+0.12}^{-0.11}$ dex) for CO(1–0) (CO(2–1), CO(3–2)). Note the inverse scaling between disk and nondisk, due to the balance shifting between the two components for a constant total luminosity. To first order, the same percentage changes apply to the other quantities mass, outflow rate, energy, and momentum.

Appendix C: Disk/Nondisk Separation: pV Diagrams

Figure 12 shows all pV diagrams for the slices defined in Figure 4. For the discussion on these diagrams, see Section 3.

Figure 12.
Standard image High-resolution image
Figure 12.

Figure 12. Position–velocity diagrams for all slices defined in Section 3 and Figure 4 for CO(1–0), CO(2–1), and CO(3–2) from the left to right columns. A description of the overlays is given in Figure 5.

Standard image High-resolution image

Footnotes

  • 11 

    The term streamer here denotes structures with a high aspect ratio that are typically oriented roughly perpendicular to the disk and often show a velocity gradient.

  • 12 

    For details, see NAASC memo 117 by the North American ALMA Science Center (NAASC) at http://library.nrao.edu/public/memos/naasc/NAASC_117.pdf.

  • 13 

    Adjusting from the distance D = 2.5 pc used by Mauersberger et al. to the D = 3.5 pc assumed here.

  • 14 

    We follow IAU resolution B2 that defines the bolometric magnitude in absolute terms and eliminates the dependence on the variable magnitude of the Sun.

  • 15 

    Assuming a Salpeter-like IMF (α = 2.35, mass range 0.1–100 M, Z = 0.008). The usual uncertainties related to the shape, upper mass cutoff, and influence of binary stars apply.

Please wait… references are loading.
10.3847/1538-4357/ab2d9c