The LWS is a spectrometer for medium and high resolution spectral observations
in the wavelength ranges 43-196.7 and 47.0-196.7 m respectively. The
instrument has a 1.65' aperture, which corresponds to the diffraction limit at
118
m. A four position aperture wheel is
used to select the observing mode of the instrument. This wheel has one closed
position, one open position for grating observations (43-196.7
m) and
two tunable Fabry-Pérots for short (47-70
m) and long (70-196.7
m)
wavelength observations. To observe the full wavelength range 10 semiconductor
detectors are used covering 10 adjacent wavelength bands. The instrument has
two principal observing modes, a medium resolution mode and a high resolution
mode.
To give some examples of the performance of LWS, in medium resolution grating
mode an observation at 100 m of a 10 Jy object (e.g. a star) will take
4.35 sec. per spectral point, giving a S/N ratio of about 50 per spectral
point. Assuming the spectrum is observed with four points per spectral
resolution element (260 points in total) a full spectrum would then take 1508
sec (25m8s), including instrumental overheads. A high resolution FP observation
of a 5*
W/m
line at 63
m on a 373 Jy continuum (e.g. a
star forming region with strong continuum and line fluxes) will take 23.5 sec
per spectral point, giving a S/N ratio of 21 on the total flux and 10 on the
line. The total time for a line scan with 4 spectral resolution elements on
either side of the line, and 4 spectral points per resolution element (36 in
total) would be 1128 sec (18m48s), again including instrumental
overheads.
The LWS Flight Model has been delivered to ESA and is being used for the Integrated Module Tests at DASA. The LWS instrument has been useful for detecting the dark background radiation at long wavelengths within the ISO cryostat, and determining its spectral shape. The LWS Flight Spare is currently being tested in the Cryogenic Test Facilities in the Rutherford Appleton Laboratories (Chilton, UK). Tests are going well and the overall performance of the model is satisfactory. The model is also used to test the commanding of the instrument for calibration observations.