The OM can operate in the two modes listed in Table 25. These allow either imaging or fast photometry or both simultaneously.
|Imaging||Mosaic of 2-D imaging windows with long exposure times ( s)|
|Fast||High time resolution, providing 2-D time-sliced images over small areas.|
The Image Mode emphasises spatial coverage at the expense of timing information. Images can be taken at the full sampling of the instrument or binned by a factor of 2 to yield a resolution element on the sky of approximately 0.5 or 1.0 seconds of arc. The maximum total size of the science windows is determined by the memory available in the Data Processing Unit DPU. A single Image Mode window binned by a factor 22 can be up to 976960 detector pixels, which results in a 488480 binned pixel image being stored in the DPU. At full sampling (with no binning) the window can be up to 652652 pixels. The trade off is that the images with unbinned pixels take more memory and therefore more telemetry when downloading the data.
The maximum allowed integration time for an OM imaging mode exposure is 5 ks. Since the OM in its imaging mode produces accumulated images, there is no timing information attached to individual incoming photons.
Any drift in the pointing direction of the spacecraft is corrected in the image by tracking guide stars.
The operating modes for Imaging consist of a combination of windows (up to five) covering different areas of the detector, or a full frame mode where the whole field of view can be observed.
The maximum allowed integration time for an exposure with one Fast mode window is 4.4 ks, and 2.2 ks if two Fast mode windows are used simultaneously.
For critical time coverage, it has to be taken into account that during ground station handovers OM exposures are interrupted for 1800 sec.
Fast mode data can be acquired at the same time as image mode data. The default configuration for fast mode includes a large image window, in which the fast mode one is embedded. In case of User Defined windows, it is recommended to include an image mode window of bigger size than the fast mode one that includes the later.
Each mode has a specific overhead, i.e., time needed for
the instrument set-up, before the actual science exposure can
start. For both the above OM modes this overhead includes also the
reference frame exposure. In addition, about 1000 s are needed before
starting the OM exposures for the field acquisition of the satellite
The reader is referred to § 4.5.2
for a general discussion of the impact of instrumental overheads
on the planning of an XMM-Newton observation, and to the
XRPS User's Manual
for a detailed description of the OM overheads.
An interactive web tool is available at the MSSL web page:
http://www.mssl.ucl.ac.uk/www_astro/xmm/om/om_tool_current.html, which may help the user to better handle and understand OM windows and operational overheads.