INTEGRAL AO-1 Core Programme (Guaranteed Time)

The Core Programme consists of three elements, which are in priority

(1) A Deep exposure of the Galactic Central Radian (GCDE): 4.30 x 106 sec
(2) Regular scans of the Galactic Plane (GPS): 2.30 x 106 sec
(3) Pointed observations of selected sources: 2.72 x 106 sec
Full details on the core programme can be found here. A summary is given below.
 
(1) Deep exposure of the Galactic Central Radian (GCDE):
The central radian of the Galaxy will be observed using a pattern of 4 rectangular pointing grids symmetric around the Galactic Centre with a pitch of 2.4 deg.

Grid 1: 17 x 26 points (442 points), l = +/- 30 deg, b = +/- 19.2 deg, Grid 2: 8 x 25 points (200 points), l = +/- 29.8 deg, b = +/- 8.4 deg
Grid 3: 8 x 26 points (208 points), l = +/- 30.0 deg, b = +/- 8.4 deg, Grid 4: 9 x 25 points (225 points), l = +/- 28.8 deg, b = +/- 9.6 deg

This pattern is chosen to minimise SPI imaging artefacts and to optimize the IBIS sensitivity towards the Galactic plane. Within |b| < 10 deg the grids are shifted relative to each other by 1.2 deg (1/2 pitch). By using 4 grids the exposure ratio of the areas within |b| < 10 deg and |b| > 10 deg becomes 4:1. Slew time between points is conservatively assumed to be ~ 200 s using the specification value for a 6 deg open loop slew (300 s). The nominal exposure per point is 30 minutes. 
The total duration of one cycle (one pattern of 4 grids including slews) is estimated at 2.15 x10^6 s. Within the total time allocation for the GCDE one cycle will be performed twice per year. Due to visibility constraints, the entire pattern never can be scanned at once, but ISOC will schedule a series of subscans (rasters). 


 
 
(2) Regular scans of the Galactic Plane (GPS): 
The baseline set of parameters describing the GPS scans are the result of an optimization process taking spacecraft and ground segment elements, instrument characteristics and scientific objectives into account. Basically the scans will be performed once a week by executing a "slew and stare" manoeuvre of the spacecraft across the visible (accessible) part of the Galactic plane with an extent in latitude up to +/-10 deg. The angular distance between two "staring points" along the scan path is 6 deg, the extremes in latitude of the pointings are at b = +/- 6.45 deg. The scans will be performed in a sawtooth pattern with an inclination of 21 deg with respect to the Galactic plane, each subsequent scan being shifted by 27.5 deg in galactic longitude. A schematic view of two consecutive scans is shown in the Figure below. The sum of all GPS scans during a year provides a set of grid points ("dither pattern") which facilitates the imaging with SPI. The accessible part of the Galactic plane depends on viewing constraints, including the solar aspect angle, and on the season of the year. 

(3) Core Programme Pointed Observations (sorted with target RA in ascending order):
 

For year 1 (AO-1) the CP guaranteed time for pointed observations (total for year 1 = 2.72 x10^6 s, see above) is split up as follows:

Proposal ID
click on ID for abstract
Title
PI
Target
RA (J2000) [deg]
Decl (J2000) [deg]
Time [ksec]
0110009 INTEGRAL CP Observations of the Vel region ISWT Vela region
133.189859
-44.585333
1000
0110011 INTEGRAL CP TOO Observations: Mrk 501 ISWT Mrk 501
253.467917
39.760194
300
0110006 INTEGRAL CP Observations of TOOS: Galactic transient events ISWT GX 339-4
255.706250
-48.789722
300
0110006 INTEGRAL CP Observations of TOOS: Galactic transient events ISWT 1E 1740-2942
266.011250
-29.723611
300
0110010 INTEGRAL CP Observations of TOOs: Superluminal sources ISWT GRS 1915+105
288.797917
10.945556
200
0110010 INTEGRAL CP Observations of TOOs: Superluminal sources ISWT GRO J1655-40
298.501042
-39.845833
200
0110006 INTEGRAL CP Observations of TOOS: Galactic transient events ISWT Cyg X-1
299.590333
35.201611 
300
0110006 INTEGRAL CP Observations of TOOS: Galactic transient events ISWT Cyg X-3
308.110833
40.952500
300
0110001 INTEGRAL CP observations of TOOs: SNe (Ia and local type II) Integral Science Working Team (ISWT) SN Ia 
any
any
2000
0110001 INTEGRAL CP observations of TOOs: SNe (Ia and local type II) ISWT SN II
any
any
3000
0110005 INTEGRAL CP observations of TOOs: Classical Novae ISWT Classical novae
any
any
1200
0110002 INTEGRAL CP TOO observations: Previously unknown X/-gamma-ray transients ISWT New X-/gamma-ray transient
any
any
1600

Strategy for the selection of unknown and known transient sources:
These events can be triggered from INTEGRAL detections of  a "high state" during the GPS and/or GCDE observations or from observations external to INTEGRAL (e.g. ground-based optical telescopes) and are considered as TOO follow-up observations.
The following strategy will be applied: the allocation of 1.7 x 10^6 s for year one shall be used for either the following unknown transient sources of the following type:

whatever TOO event comes first. The trigger criteria (see AO1 documentation) have been defined so that the events listed above become scientifically an exceptionally unique - and for INTEGRAL important - target.

Note on TOO follow-up observations:
It is expected that most TOO events will be detected during the Core Programme elements GPS and GCDE: this is one of the main reasons to perform the GPS and GCDE during the entire mission. TOO follow-up observations are scientifically important for INTEGRAL and a situation should be avoided where they cannot be scheduled because a specific time allocation (e.g. CP pointed observations for TOO follow-up observations) has been formally exhausted. Therefore, if at any time during an observation period of one year -- corresponding to one INTEGRAL AO cycle -- a TOO follow-up observation triggered by a detection in GPS and/or GCDE data is scheduled and executed and if the CP allocated time for TOO follow-up observations is already exhausted, then the data of the entire field-of-view of that follow-up observation will be made publicly available immediately, unless a AO-1 accepted proposal exists (see "General Programme", above). See also AO-1 documentation on "Science Data Rights" for full details.

It is understood that some flexibility should be kept by the ISWT in case a major ("once in a lifetime") TOO event (e.g. close-by SN) occurs and no or insufficient CP time for follow up observations is available anymore because the ceiling has been already reached. In this case the ISWT could review the priority assigned for the GCDE and GPS and, if available, probably re-assign remaining time from these CP elements. This would be an exception to the routine case where the execution of TOO follow-up observations will be decided by the Project Scientist. See also AO-1 documentation on "Guaranteed Time" for full details.


The General Programme (open time) observations, which complete the INTEGRAL observing programme, can be found here.



Last Updated on 17.08.2001
ESA/ISOC