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Astron. Astrophys. 350, 529-540 (1999)
3. Analysis of molecular emission
To understand the origin of the observed strong molecular emission,
we first want to derive the physical parameters, averaged over the
rather large LWS beam ( 75"), which
characterises the different gas components. For this purpose, the line
emission from CO, H2O and OH have been analysed by
solving the radiative transfer in the line simultaneously with the
level populations, under the Large Velocity Gradient (LVG)
approximation in a plane-parallel geometry. Given the average nature
of the observed emission and the uncertainty on the exact geometry
involved, we did not attempt to consider a more realistic geometrical
model. In principle, the emission from warm dust could be efficient in
the radiative excitation of H2O and OH; however, the
influence of the local radiation field has not been taken into account
in the radiation transfer calculations considering that the continuum
source has a temperature of about 30 K and a dust opacity of only 0.07
at 200µm (Barsony et al. 1998), while gas
temperatures in excess of 500 K are implied by our observed lines (see
Fig. 6).
![[FIGURE]](img33.gif) |
Fig. 6. Energy level diagram of H2O with the transitions observed by LWS in L1448-mm and their wavelengths in microns indicated.
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In these approximations, the expected flux of a transition at
frequency is given by:
![[EQUATION]](img36.gif)
where is the spontaneous
radiative rate, is the fractional
population of the upper level of the transition,
is the number density of the
considered molecular species, is the
depth of the emitting region subtending a solid angle
, and
is the angle-averaged escape
probability which depends on the line optical depth
through the relationship (valid for
a plane-parallel geometry, Scoville & Solomon 1974):
![[EQUATION]](img44.gif)
The optical depth can be expressed as:
![[EQUATION]](img45.gif)
where is the velocity gradient in
the region and and
are the populations and the
statistical weights of the upper and lower levels respectively.
If we assume an homogeneous slab where the total velocity
dispersion is this last expression
can also be written:
![[EQUATION]](img50.gif)
making explicit the dependence on the column density
( ) of the particular molecule.
The fractional population is given by the equations of the
statistical equilibrium which, for a collisionally excited molecule,
depend on the local temperature and density as well as on
.
From the above expressions we can see that the line intensity
depends on several free parameters (temperature, density, size and
depth of the emitting region, velocity dispersion) some of which are
related together, and thus difficult to be simultaneously constrained
even with the large number of observed lines. However, the
high-J CO lines are likely to be optically thin
( ), in which case their relative
ratios depend only on the excitation temperatures and densities. In
addition, the H2 lines, being optically thin and
thermalised, can further constrain the gas temperature. The
temperature and density derived in this way can then be used as fixed
parameters in modelling the water and OH lines, which are very
sensitive to opacity effects because they have their energy levels
connected by strong radiative transitions.
3.1. CO and H2
The downward collisional rates for CO levels with
60 and
100 K were calculated using the
coefficients taken from McKee et al.
(1982), while the upward rates were computed using the principle of
detailed balance. Radiative decay rates were taken from Chackerian
& Tipping (1983). If we look at fluxes of the observed CO lines
plotted as a function of the upper level rotational quantum number
(Fig. 7), we note that the transitions with J=24, 25 and 26
have flux levels which are too high, compared to the lower
transitions, to be excited in the same gas component. We have
therefore attempted only to fit the transitions with
21. From their ratios we derive a
temperature ranging from 700 to 1400 K and a density in the range
3 104 to 5 105 cm-3. These limits
were obtained after considering all the model fits which were
compatible with the errors associated with the lines. In Fig. 7 we
also report the J=2 1
measurement taken from Bachiller et al. (1990): we see that both the
intensity integrated over all velocities (open triangle) and the
contribution just of the EHV gas (open circle) lie inside our
considered parameter range. In particular, temperatures greater than
1400 K would not agree with the total flux in the
J=2 1 line while the 700 K fit
already miss the J=2 1
completely; temperatures lower than this value would also fail to
reproduce both the lower and higher J lines observed by LWS,
giving rise to curves narrower than the observed flux
distribution.
![[FIGURE]](img61.gif) |
Fig. 7. Model fits through the observed CO lines. The range of temperatures and densities compatible with the observations are indicated. The total flux in the J=2 1 line from Bachiller et al. (1990) is also reported (open triangle) together with the J=2 1 emission relative only to the EHV component (open circle). The higher observed J lines (J=24, 25 and 26) have fluxes too high to be fitted by the same parameters as the other lines, suggesting the presence of a second component.
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Given the high uncertainty on the flux determination of the
J=24 and 26 lines due to their blending with the much stronger
H2O lines (see previous section), we have not
attempted to fit the second component. However, the fact that it
should peak at J 24, indicates
that its temperature cannot be lower than about 2000 K.
The analysis of the H2 (0-0) lines gives a further way
to constrain the gas temperature. Indeed, these lines originate from
quadrupole transitions and are therefore optically thin. In addition,
they have critical densities lower than
104 cm-3 1,
implying that they are very quickly thermalised; their ratios can
therefore be used to directly estimate the gas temperature. This can
be better visualised in a rotational diagram (Fig. 8), where the
natural logarithm of , the column
density for a given upper level divided by its statistical weight, is
plotted against the excitation energy of the upper level. To construct
this diagram, the spontaneous radiative rates were taken from Turner
et al. (1977), and an ortho- to para- H2 equal to 3 was
adopted. For a Boltzmann distribution, the slope of this plot is
inversely proportional to the kinetic temperature of the gas. We note
that the three detected lines were all observed with the same beam
size, and therefore no beam filling correction is needed.
![[FIGURE]](img68.gif) |
Fig. 8. H2 excitation diagram. The open circles are the observed line fluxes to which a dereddening of =5 mag has been applied, while open squares are dereddened with =11 mag
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The S(3) line at 9.7 µm is particularly sensitive
to extinction corrections, lying in the middle of the silicate
absorption feature. An average visual extinction of about 5 mag was
estimated towards the region covering the entire outflow (Bachiller et
al. 1990), but of course the reddening could be much larger than this
value on smaller scales, particularly in the surroundings of the mm
source. Given the fact that the S(4) and S(5) lines are much less
affected by reddening than the S(3) line, we can make a rough estimate
of the extinction correction by imposing that the S(3) transition
should lie on the same line as the other two transitions in the
excitation diagram. In this way we estimate
11
mag. Fig. 8 shows the derived excitation temperatures both assuming
=5 mag and
=11 mag. Given also the uncertainty
associated with the measurements, a range of temperatures from 1300 to
1700 K can be deduced. Therefore, in the assumption that the
H2 lines are emitted in the same region as the CO lines, a
temperature between 1300 and 1400 K would be favourite as the
best estimate to simultaneously reproduce the H2 and the CO
observations. The corresponding density values from the CO fits would
in this case range between 3 and 6 104 cm-3.
However, given the different beam sizes of the LWS and SWS
instruments, the possibility that they are actually tracing different
gas components cannot be ruled out. We will therefore conservatively
assume that CO temperatures as low as 700 K cannot be excluded.
3.2. H2O and OH
Assuming that the water lines originate in the same region as the
CO lines, we can take the temperature and density as derived from the
CO analysis to model the observed H2O fluxes. We will
in particular consider the two extreme conditions derived from CO,
1400 K and
104 cm-3, and
700 K and
105 cm-3,
referring to them as the "high" and "low" temperature cases
respectively. The water spectrum has been computed considering 45
levels for both the ortho and para species (i.e. considering the
levels up to excitation temperatures of
2000 K) and adopting radiative rates
taken from Chandra et al. (1984) and H2O-H2
collisional rates from Green et al. (1993). We assume an ortho/para
abundance ratio of 3, equal to the ratio of the statistical weights of
their nuclear spins.
Having fixed the temperature and density, we see from Eqs. (1), (2)
and (4) that the other parameters affecting the absolute flux
intensity of the water lines are the velocity dispersion, the
H2O column density and the projected area of the emitting
region. The optical depth in the lines is proportional to
N(H2O)/ and since
the ratios of different lines depend on their relative optical depths
through the escape probability (Eqs. [2] and [4]), we can use them to
constrain a value of
N(H2O)/ . The
dependence of the line ratios on this parameter is shown in Fig. 9 for
two different sets of lines. From the figure it appears clear that a
unique value of
N(H2O)/ can be
effectively derived from a single ratio providing that the opacity of
the considered lines is neither too high
( ) so that their absolute intensities
approach the blackbody value, nor too low
( ) that their relative ratios become
independent from the column density. The best fit consistent with all
the observed ratios gives
N(H2O)/ =
2 1016 cm-2 km- 1 s for either the
"high" and "low" temperature cases. A comparison of the observed line
fluxes with those predicted by these models is shown in Fig. 10. We
see that both cases reproduce quite well the observations, reflecting
the difficulty in determining the physical parameters of the emission
using the water lines alone; however, the "high" temperature case
seems to give a slightly better agreement with the data, especially
because it is able to reproduce the observed 179.5
µm line, which is the strongest line observed in the
spectrum.
![[FIGURE]](img80.gif) |
Fig. 9. Ratio of intensities of the 303-212 174.6 µm to the 221-110 108.1 µm (upper panel) and of the 221-212 179.5 µm to the 505-414 99.5 µm (lower panel) H2O lines, as a function of the N(H2O)/ parameter for a gas temperature T= 1400 K and a volume density =3 104 cm-3. The straight line indicates the observed value while the dashed region delimits the range of uncertainty.
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![[FIGURE]](img82.gif) |
Fig. 10. Comparison of the modelled H2O line fluxes (triangles and squares indicate the lines in the ortho and para form respectively) with the observations (open circles) in the two extreme conditions derived from the CO fit. We note that the theoretical fluxes for the lines not observed in the LWS spectrum are all below the detectability threshold.
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The absolute line intensity depends on both
N(H2O) and , which
can be independently derived once a linewidth
is assumed. To estimate
we assume that the observed emission
is related to the outflow activity taking place in the close
environment of the millimeter source. This has been traced in many
different molecular lines (e.g. H2, CO, SiO), having widths
ranging from 20 to 50 km s-1. Taking this range of values
we derive a water column density of
(0.4-1)1018 cm-2; the projected area of the
emitting region in the "high" temperature regime is then (50-120)
arcsec2 (i.e. 7-12" diameter assuming a single
emitting region), implying that about 2% of the LWS beam is filled
with emitting gas. Adopting this source size, the CO column density
can be now estimated from the observed CO line fluxes, giving
N(CO)= (0.6-3)1017 cm-3 (a range which
also takes into account the absolute flux calibration errors). We find
therefore that the H2O/CO abundance ratio is
5. Hence, for the standard CO
abundance of 10-4, the water abundance is
5 10-4, implying an
enhancement with respect to the ambient gas of a factor
103 (Bergin et al.
1995).
On the other hand, assuming the "low" temperature regime a more
compact region of 3-5" of diameter is derived from the water
lines; since however the intrinsic CO line intensity of the considered
transitions is higher than in the "high" temperature case, the implied
CO column density is similar in the two cases and consequently the
H2O/CO ratio remains almost unchanged. This makes us
confident that the derived value of the water abundance does not
depend significantly on specific values adopted for the physical
conditions and projected area, the only assumption affecting this
value being that CO and water are emitted by the same gas
component.
Finally, we also remark that our model predicts a population
inversion in the 22 GHz
-
transition, which has been detected in the form of strong masering
spots aligned with the stellar outflow (Chernin 1995), but we are
unable to reproduce the large line luminosity observed; the 22 GHz
maser is however localised in dense (
106) and very compact regions probably having the optimal
geometry for producing the strong masering, while the LWS observations
probe emission on larger scales.
Very high abundances of gas-phase H2O have so far been
estimated only for the Orion region (Harwit et al. 1998) but never in
low mass protostars similar to L1448, since the typical values in
these sources are of the order of (1-5) 10-5 (Liseau et al.
1996; Saraceno et al. 1998; Ceccarelli et al. 1998). In this respect,
L1448-mm seems to have an exceptionally high water abundance,
indicating that the processes responsible for the production of
gas-phase water are particulary efficient here. We will discuss this
point further in the next section.
Finally, adopting the same parameters as derived from the above
analysis also for OH, from the observed 119 µm flux
we deduce a column density N(OH) of
(0.7-1.3) 1016 cm-2 and therefore an
X(OH) 10-5, i.e.
2 10-2 times the water abundance. For the molecular
parameters and assumptions in the modelling of the OH, we refer to
Giannini et al. (1999).
Table 3 summarises the derived quantities for the observed
molecular species.
![[TABLE]](img87.gif)
Table 3. Ranges of physical parameters for the molecular emission.
Notes:
a) The given range takes into account the lower and upper limits for the emitting region deduced by the different models (see text).
b) Obtained assuming the same emission area as the other components; see text for a discussion on this point.
3.3. The N(H2) column density
The absolute intensities of the observed H2 lines can in
principle be used to derive the H2 column density if the
beam filling factor is known. Adopting the hypothesis that the
high-J CO and H2 pure rotational line emission is
fully enclosed within the relatively smaller SWS beam, we can use the
size of the emitting region derived from the above analysis to
estimate the N(H2) of the warm gas, obtaining a
value of about 1019 cm-2. When compared with the
estimated CO column density, this value would imply a CO/H2
abundance of 10-2. This
result does not in fact depend on the specific model adopted; a direct
measure of the CO/H2 abundance ratio in the warm gas can be
independently given simply by comparing the ratio of two observed
lines emitted in the same conditions. Indeed, both the high-J
CO and the H2 lines are optically thin and therefore their
ratio is directly proportional to the ratio of their relative column
densities. Measuring the ratio for different sets of lines, we always
obtain a value of CO/H2 of the order of 2 10-2.
One possible explanation for this anomalous abundance ratio (the
interstellar CO/ H2 abundance is of the order of
10-4, while in dense cores some of the CO can be depleted
on grains, further reducing this value, see e.g. van Dishoeck et al.
1993) could be that the region strongly emitting the molecular lines
observed by the LWS, has been totally or partially missed by the
smaller SWS beam. This in turn would imply, giving the low
beam-filling derived for the LWS observations, that the region of
emission is not located in the center of the two beams, i.e.
coincident with the mm source.
Alternatively, the extinction in the region could be much higer
than assumed in our analysis. An
value of about 250 mag would be necessary to increase the
H2 S(4) and S(5) observed fluxes by a factor of one
hundred, which is needed to find a CO/H2 abundance ratio
similar to the commonly assumed interstellar value. Such a high
extinction, which is found only if the observed lines originate from
very close to the protostar itself, would strongly affect the
(0-0) S(3) line intensity, causing it to deviate too much from the
straight line in the rotational diagram. Inconsistencies would be also
found with the upper limits of the S(1) and S(2) lines, which, by
contrast, are not greatly affected by a large amount of
extinction.
A different interpretation could be that in the considered region
the hydrogen is not fully molecular but part of it is present in
atomic form. This circumstance could happen for instance in
protostellar winds, where a significant fraction of atomic hydrogen
can be present even if the heavy atoms are processed into molecules
(Glassgold et al. 1991). Alternatively, also in the presence of
dissociative shocks a significant part of the post-shock gas can be
composed of hydrogen which is mainly in atomic form (Hollenbach &
McKee 1989). That the flow from young stars can be characterised by an
appreciable amount of atomic hydrogen has indeed been demonstrated by
the detection of the 21 cm hydrogen line associated with high-velocity
molecular outflows (e.g. Lizano et al. 1988).
The different possibilities will be discussed in Sect. 5.
© European Southern Observatory (ESO) 1999
Online publication: October 4, 1999
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