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The layout of the IDS spectrograph is shown in Figure 3.1. The following components can be discerned:
m (0.216 arcsec) to 1.745 mm 
    (9.43 arcsec) in steps of 5 
m (0.027 arcsec).  The entire slit 
    assembly can be removed, if required.  Dekker plates are interchangeable 
    in sets; each individual set consisting of 8 apertures and a clear 
position. Several standard dekkers, incorporating
    single slots, pairs of slots, a ``comb'', and a coronographic set-up, are
    always available.
    A multislit unit is also available. This consists of ten parallel 
    slitlets, each 16s long with a 7s gap between each pair and with 
    a fixed width of 270 
m (1.46s  at the Cassegrain focus). Each 
    slit can be moved perpendicular to the slit orientation by up to 
    1.6 
  in either direction. With FOS-1 a useful field of 
    4 
 by 3 
 can be covered, whereas the IDS has a smaller field 
    of 4 
by 1 
 .  A program is available for finding the optimum 
arrangement and typically one needs 20 or 30 objects in the field to make use 
    of all 10 slits. Astrometry to within 0.3s is needed to use the unit 
    effectively. There is only one module that has to be preset using
    a Coradograph xy table in the INT building. Clusters of objects spread 
    over less than 1 
 are less likely to benefit as they are too small. 
    To install the multislit assembly, the
conventional Cass cluster slit assembly is replaced by a similar one 
which holds the multislit module or a long-slit equivalent. This instrument
change requires lowering the IDS and is a daytime operation.  The long slit 
module allows observations to continue while the multislit module is being 
preset with the Coradograph for a new field. The device should not be regarded
as a general purpose multiobject coupler but rather as a special purpose 
addition to the INT Cassegrain cluster instrumentation. 
 See  Using the multislit unit at the 
INT Cassegrain focus (R. Ellis et al. 1986)  for more information.
 60 mm 
 2 mm and made from Schott glass. The 
    wavelength dependence of the
    transmission of these filters is shown in figures 2.5 and 2.6. The copper 
    sulphate filter cuts out the part of the spectrum from 600 - 650 nm 
    redwards and is usually employed to block the red leak of the UG11 filter
or to remove the FOS-1 first order. 
    The neutral density filters 
    below the slit provide a choice of ND = 0.5, 1.0 and 1.5.
    Note that the use of filters below the slit makes it necessary to
    refocus the spectrograph.
    Along the direction of the slit (i.e. perpendicular to the dispersion 
    direction), the focal lengths of 235 and 500 mm imply slit to detector 
    reduction factors of 5.43 and 2.55 respectively, and hence scales 
    at the detector of 29.4 and 13.8 arcsec mm
.
    Along the dispersion direction, the slit to detector reduction factor
    is more complicated, since it depends on the grating angle. Tables 3.1 
    and 3.2 give the slit width in arcsec which projects to 30 
m at the 
    detector, when each grating is used at its central wavelength.
    Tables 3.1 and 3.2 also list the dispersion provided by each grating and 
    camera combination. It can be seen that a wide range of dispersions
    is available, from 7 Å mm
 to 270 Å mm
.


 128 mm. A wide selection is available,
    and some of the important characteristics of each grating are summarised
    in Tables 3.1 and 3.2. The efficiency of the gratings as a function of 
    wavelength is shown in Figure 2.4. Grating changes can be made during 
    the night by support staff.
    and 
    blazed at 4800 Å, can be inserted into the collimated beam in the 
    235 mm camera to provide a cross-dispersion option. This is 
   used in conjunction with an R150 echelle grating, which is blazed at 
   2.7 
m. The FOS-1 dekker mask is used to limit the slitlength to 25
   arcsec in order to avoid order confusion.
   The wavelength range for the CCD and dispersion provided by this grating in 
each order, for a grating angle of 60 
, are summarised in Table 3.3. There
are no gaps in wavelength coverage with the IPCS.
   The CCD is not normally considered the detector best suited to use with the 
   cross-disperser, because part of the wavelength coverage is lost between
   the orders due to the physical size of the chip. However, it is usually
possible to adjust the grating angle in the range 59.5 
 - 60.5 
  so as to
ensure that all interesting spectral features are placed in the chip.
Besides the 
   advantages typical of CCDs, the combination of GEC chip and cross-disperser, 
   seems to have a higher sensitivity than the combination of
   IPCS and cross-disperser.  13 counts/sec/Å were obtained for a 
   m
=11.9 star at an airmass of 1.32 with the CCD. 1 count/sec/Å
therefore, can be expected for a m
=14.8 at an airmass of 1.0. This count
rate corresponds to a m
=13.9 with the IPCS, but of course the IPCS's 
quantum efficiency is much lower at 5500 Å than that of the CCD.
The central wavelength and wavelength coverage in Å can be obtained for 
each order 
 as
and


 around the optical
axis (or exchanged), and the control software to be reinitialized. Note that if
you only specify a detector to be on one camera in your proposal, you cannot 
guarantee what will be on the other (e.g. it might be in use on another 
telescope). If you need both cameras, you have to specify that well before
your run.