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Recipes for the planning of proposals using SWS

 

For each SWS AOT calculation  the procedure is first to determine in which AOT band the desired spectral region occurs; secondly to calculate the detector reset time tex2html_wrap_inline2408 necessary to reach the desired SNR; and thirdly to determine the number of integrations necessary to cover the desired wavelength region. To this cause it is necessary to carefully read the previous chapters, and in particular to take notice of
- the AOT band structure given in Tab. 2.1 (p. gif)
- chapter 3 in full,
- noise parameters as given in Tab.5.2 (p. gif) and Tab.5.3 (p. gif), and
- spectral response figures as given in Fig. 5.3 (p. gif) to Fig. 5.8 (p. gif) and Fig. 5.10 (p. gif).

Tab. 6.3 (p. gif) describes details of each SWS AOT.

Parameters used in this section are:
  tex2html_wrap_inline2410 : step size in scanner steps (a resolution element covers about 6 scanner steps)
tex2html_wrap_inline2930 : number of samples taken from a single spectral resolution element
tex2html_wrap_inline2412 : number of scans
tex2html_wrap_inline2934 : number of steps
tex2html_wrap_inline2714 : dark current noise
tex2html_wrap_inline2710 : detector read noise
tex2html_wrap_inline2718 : shot noise
R: nominal grating mode resolution
S: signal strength in tex2html_wrap_inline2404 V/s
tex2html_wrap_inline2948 : source flux density in Jy
SNR: signal-to-noise ratio
tex2html_wrap_inline2408 : detector reset time in sec

Some general points of interest are:
- per AOT up to 64 observations can be requested. If more observations are desired, an additional AOT request has to be defined;
- in all AOT's simultaneous use of SWS LW and SW sections is arranged automatically;
- at the ISO observatory, before execution of an F-P AOT, a correction of the radial velocity  for the projected component of the earth's orbital motion is introduced ;
- where peak flux density estimates are requested, they are needed to select amplifier gain settings. A factor of four in accuracy is sufficient to prevent saturation;
- observers are charged for the total time for execution of each AOT. This so-called Target Dedicated Time (TDT)  includes actual on-source integration time, overheads for internal calibrations (excluding wavelength calibration), and satellite overheads for slewing and pointing;
- all wavelength calibrations are scheduled separately by the Science Operations Team.


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Next: Merging: simultaneous use of Up: AOT Cookbook Previous: Overheads

SWS Consortium
Wed Aug 7 17:20:29 MET DST 1996