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    Instruments

    Baseline instrument concept

    NOTE: In March 2011 ESA announced a new way forward for the L-class candidate missions: IXO, EJSM-Laplace and LISA.
    At this time the IXO concept ceased to be a candidate and ESA, along with the scientific community, is now investigating to what extent a European-led mission could preserve the original science case of IXO. The new study is called ATHENA (Advanced Telescope for High ENergy Astrophysics).

    In order to fulfil the IXO science requirements the following baseline instrument complement has been adopted:

    1. Wide Field Imager (WFI)
    2. Hard X-ray Imager (HXI)
    3. X-ray Microcalorimeter Spectrometer (XMS)
    4. High Time Resolution Spectrometer (HTRS)
    5. X-ray Polarimeter (X-POL)
    6. X-ray Grating Spectrometer (XGS)

    The baseline instrument payload (see table below) is used during mission studies to scope the key elements of the mission and to ensure that the scientific requirements of the mission can be achieved. An Announcement of Opportunity will be issued at a later date inviting the community to propose specific instruments for the observatory.

    Above: Schematic illustration of the location of the instruments. Credit: ESA

    Left: Top view of the IXO instrument module;

    Below (left): assembly view of the IXO instrument module;

    Below (right): geometrical mathematical module. Credit: ESA

    Summary of the baseline instrument payload

      WFI HXI XMS
    Detector type Si APS (DEPFET) CdTe + Si strip detectors Micro-calorimeter / TES
    Operating temp 210 K 253 K 50 mK
    Cooling Radiator (+Peltier) Radiator Closed cycle coolers / ADR
    Detector size (mm) 102.4 × 102.4 70 × 70 31.2 × 31.2
    Energy Range (keV) 0.1 - 15 10 - 40 0.2 - 6
    Energy resolution (FWHM) 70 eV @ 1 keV 1 keV @ 40 keV 3 eV @ 6 keV
    Pixel size (µm) 100 220 300 (& 600)
    No. pixels in one direction 1024 320 strips 40 (+ 32)
    Field of View (arcmin²) 18 12 2 (& 5.3)
    Unvignetted
    FoV (arcmin*)
    18 (diam) TBD 12 (diam) TBD 5.3 (diam)
    *: assuming a circular field of view

    Summary of the baseline instrument payload (continued)

      HTRS X-POL XGS
    Detector type Silicon Drift Diodes (SSD) Gas Pixel Detector CCD
    Operating temp 253 K 290 K 170 K
    Cooling Radiator None Radiator
    Detector size (mm) 16.8 (Hexagonal) 16 × 16 741 × 28.8
    Energy Range (keV) 0.5 - 20 2 - 10  0.3 -1
    Energy resolution (FWHM) <200 eV @ 6 keV 1200 eV @ 6 keV E/ΔE = 1250
    Pixel size (µm) 2400 50 18
    No. pixels in one direction 7 320 40960
    Field of View (arcmin² ) 2.8 (Hexagonal) 2.8 n/a
    Unvignetted FoV (arcmin*) 2.8 (diam) 2.8 n/a
    *: assuming a circular field of view

     

    Wide-Field Imager (WFI)

    Last Update: 07 Feb 2012

    • Shortcut URL
    • http://sci.esa.int/jump.cfm?oid=43937
    • Related Articles
    • Baseline instrument concept
    • Wide-Field Imager (WFI)
    • Hard X-ray Imager
    • X-ray Microcalorimeter Spectrometer (XMS)
    • High Time Resolution Spectroscopy (HTRS)
    • X-ray Polarimeter (XPOL)
    • X-ray Grating Spectrometer (XGS)

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