The SVOM mission, 

a new generation GRB mission

Future GRB studies must rely on the availability of a continuous flow of accurate GRB positions (to take advantage of instrumental progress), but also on the measure of many additional parameters of the GRB (e.g. redshift, E-peak, jet break time, ...) which are crucial for the understanding of the GRBs themselves and for their use as astrophysical tools.

The SVOM mission (Space-based multi-band astronomical Variable Objects Monitor) will:

  • Permit the detection of all known types of GRBs
  • Provide fast, reliable GRB positions
  • Measure the broadband spectral shape of the prompt emission (from visible to MeV)
  • Measure the temporal properties of the prompt emission (from visible to MeV)
  • Quickly identify the afterglows of detected GRBs at X-ray and optical wavelengths, including those which are highly redshifted (z>6)
  • QMeasure the broadband spectral shape of the early and late afterglow (from visible to X-rays)
  • QMeasure the temporal evolution of the early and late afterglow (from visible to X-rays)

The mission concept

The constant advances in the field of GRB studies is made possible by the increasing synergy between space and ground instruments. The SVOM mission has been designed to optimize particularly this synergy. The on-board instruments will permit the detection of the GRBs, their localization from arcminutes to arcsecondes accuracy, the study of the prompt emission, the early detection and follow-up of visible afterglows, and the primary selection of high-redshift candidates (z>6). The ground segment will permit the fast distribution of the alerts, the localization of GRBs with sub-arcsecondes precision and the multi-band photometry of the afterglow and the prompt emissions, from the visible to the near-infrared domains.

These functions will be achieved by a set of wide and narrow field instruments. Such a combination requires a very specific observation scenario, which is based on the successful experience of the Swift mission:

  1. the detection is done by a very wide field gamma-ray imaging instrument able to derive on-board localization with few arcminutes accuracy;
  2. the position is immediately transmitted to the ground segment and to the scientific community through a VHF stations network;
  3. in parallel the satellite slews rapidly and automatically (when safely possible, regarding to the pointing constraints) to position the GRB in the narrow field of view of the onboard instruments, an X-ray and an optical telescopes, which will study the afterglow and provide refined coordinates. The observations start less than 5 minutes after the detection.

The scientific objectives of the mission put a very special emphasis on two categories of GRBs: very distant events at redshift greater than 6, which constitute exceptional cosmological beacons, and faint/soft nearby events, which allow probing the nature of the progenitors and the physics at work in the explosion. These goals have a major impact on the design of the mission: the onboard hard X-ray imager must be sensitive down to 4 keV and able to compute image and rate triggers on-board, and the follow-up telescopes on the ground must be sensitive in the near infrared.



 
 
     
Mentions légales

Textes : Stéphane Basa
Mise en page: Bruno Thooris