 
 
 
 
 
 
 
 
 
 
 
  The ISOCAM instrument on board the Infrared Space Observatory ISO
   was designed to map selected areas of the
  sky in the spectral region from 2.5 to 18 m at various spatial
  and spectral resolutions.
m at various spatial
  and spectral resolutions. 
 
  With ISOCAM, spectral features at wavelengths inaccessible from the ground
  were studied.
  The morphology of objects at a scale of a few arcseconds was 
  investigated through broad and narrow band filters.  Spectral imaging was
  also possible with Circular Variable Filters (CVF) 
  at a spectral resolution of up to 
 .
.
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  The spatial resolution was determined by the diffraction limit at longer
  wavelengths, and was limited mainly by undersampling of the PSF at shorter
  wavelengths. For a 60 cm diameter telescope the diameter in 
  arcseconds  of the Airy disc (FWHM) 
  is given by 
![$\lambda/D = \lambda~[\mu{\rm m}]/3$](img21.gif) , or
, or 
  
![$ 2.4 \cdot \lambda/D = 0.8 \cdot \lambda~[\mu{\rm m}] $](img22.gif) for the first
  dark ring.  Regarding the optical performance of ISO, images of point
  sources were made, clearly showing up to the fifth Airy
  diffraction ring. A detailed description of the telescope and the
  pointing system  is given in the ISO Handbook Volume I,
  [40].
 for the first
  dark ring.  Regarding the optical performance of ISO, images of point
  sources were made, clearly showing up to the fifth Airy
  diffraction ring. A detailed description of the telescope and the
  pointing system  is given in the ISO Handbook Volume I,
  [40].
 
  ISOCAM provided imaging capabilities across a field of view of up to
  3 diameter. It consisted of two optical channels,
  used one at a time,
  each of which containing a
 diameter. It consisted of two optical channels,
  used one at a time,
  each of which containing a  pixels infrared detector
  array. The short wavelength channel (SW) operated between 2.5 and
  5.2
 pixels infrared detector
  array. The short wavelength channel (SW) operated between 2.5 and
  5.2 m; the long wavelength channel (LW) between 4 and 18
m; the long wavelength channel (LW) between 4 and 18 m. Each
  channel included lenses covering a range of magnifications (yielding fields
  of view having 1.5, 3, 6  and 12
m. Each
  channel included lenses covering a range of magnifications (yielding fields
  of view having 1.5, 3, 6  and 12
 per pixel), fixed 
  filters and CVFs.  
  During the ISO pre-flight thermal vacuum tests it was discovered that 
  the apparent output voltage of one  of the LW detector columns 
  (`column 24') was always at zero Volts. In space it was found that,
  because of the repositioning jitter in the camera wheels, the edges 
  of the array (essentially the outermost columns),  did not always receive
  sufficient light when using the 6
 per pixel), fixed 
  filters and CVFs.  
  During the ISO pre-flight thermal vacuum tests it was discovered that 
  the apparent output voltage of one  of the LW detector columns 
  (`column 24') was always at zero Volts. In space it was found that,
  because of the repositioning jitter in the camera wheels, the edges 
  of the array (essentially the outermost columns),  did not always receive
  sufficient light when using the 6
 per pixel lens.
 per pixel lens.
 
 
 
 
 
 
 
 
