Astron. Astrophys. 344, 333-341 (1999)
2. Spectral model
The spectral modelling is done using a series of "slabs" which are
set up to represent hot gas emission regions and cold gas absorbing
layers (Sidher et al. 1996, see also Pietz et al. 1998 and references
therein for similar analyses). In this work the furthestmost slab
defines the extragalactic component of the SXRB, which is taken to
have a power law source spectrum of spectral index 1.4. The next two
slabs contain a hot gas component, which we associate with the
Galactic halo, and the cold absorbing Galactic disk (see Sidher et al.
1996 for justification of this). The closest slab to us then contains
the hot gas component within the local cavity plus a small amount of
intermixed absorbing material. The radiation transfer function through
each slab is
![[EQUATION]](img2.gif)
where I i(E ) is the incident
radiation entering the shell from the outside, E is the photon
energy, (E ) is the energy
dependant absorption cross-section, n e is
the electron density, n H is the H I column
density, T is the temperature and l is the depth of the
shell. P (E,T ) is the radiative power loss function for
a plasma at a temperature T . In this work the Landini &
Monsignori Fossi plasma code has been used to model the emission from
the hot gas components in the halo and the local cavity (Landini &
Monsignori Fossi 1990). The H I absorption column in the cold gas of
the disk has been derived for each pointing direction using the Stark
catalogue (Stark et al. 1992; For a comparison with the more recent
Leiden/Dwingeloo 21-cm line survey (Hartmann & Burton 1997) see
the discussion in Sect. 3.1). The absorption cross-section as a
function of energy is taken from Morrison & McCammon (1983). To
economise on computing time the local cavity hot gas temperature is
kept fixed at log T = 5.9 with an intermixed column density of
6.6 . 1018 cm-2 (see Juda et al. 1991 and Lieu
et al. 1992). During the fitting procedure the emission measure (EM)
for both the local cavity and the halo component are treated as free
variables. In addition the temperature of the halo component is
allowed to vary. For each combination of parameters the spectrum
arriving at the telescope aperture is modelled with a 1 eV resolution
between 50 eV and 3 keV. This modelled spectrum is then convolved with
the ROSAT PSPC energy response function and the predicted spectrum is
binned at 50 eV intervals. The predicted binned spectrum is then
compared with the observed spectrum over the entire PSPC energy range
using standard .
© European Southern Observatory (ESO) 1999
Online publication: March 10, 1999
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