List of Figures

1. Overview of the INTEGRAL analysis related documents.
2. The INTEGRAL spacecraft with the payload module on the top of the service module. The coded masks for IBIS and JEM-X are located 3.2 m above the detection planes. IBIS and JEM- X detectors are inside the payload module structure. The overall dimensions of the spacecraft (excluding solar arrays which span 16 m) are 4m 6m (w h). The Sun is illuminating the payload module on the IBIS side, leaving SPI in the shadow.
3. Spacecraft & Instrument coordinate systems.
4. The INTEGRAL continuum sensitivities. Time of observation is s, the detection threshold is 3 .
5. Energy dependence of the IBIS effective area.
6. JEM-X effective area with the mask taken into account. The dashed line shows the effective area before the high voltage reduction (see text) and the full curve shows the efficiency when taking into account the effect of the electronic low-signal cutoff.
7. Schematic view of dithering patterns and instrument fully coded fields of view (FCFOV).
8. Hexagonal dithering pattern.
9. Galactic Plan Scan.
10. Schematic view of a SPI Observation Group.
11. The complete ISDC repository structure of revision 1 data.
12. The complete ISDC repository structure of revision 2 and 3 data.
13. High level directory structure of processed data repository.
14. Subdirectory structure of scw for revision 1 data. For revision 2 and 3 data, directory RRRRPPPPSSSF.VVV does not have any further subdirectories.