The SWS design and optimization of sensitivity and operational efficiency
lead to a few general restrictions that apply to all SWS AOTs:
There are minimum observing times
for all AOTs, even for very
bright sources that could formally reach very high signal-to-noise ratio
(SNR) quickly. First, there is a minimum detector reset time of
1 sec, leading to a minimum total integration time for each AOT,
depending on the minimum number of grating or F-P settings. Second,
fixed instrumental and satellite time overheads have to be added.
Details are discussed with the individual AOTs (Chapter 6).
The SWS will be used with fundamental integration times (detector
reset times ) of 1, 2 and 4 sec. The fundamental integration
time is however not selectable
by the observer; it will be set by the AOT logic based on the flux and
desired SNR provided by the observer as AOT input.
The correspondence between wavelength range and aperture size
(Tab. 2.1) is fixed and cannot be selected by the observer.
The orientation of the SWS apertures on the sky is determined by the
time of the observation. The observer cannot influence the position angle
of the long axis of the apertures, but will be supplied with the
actually achieved orientation.
For observations of solar system objects, measurements in different
entrance apertures have to be defined in separate AOT calls, i.e. as
separate observation requests.