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    Instruments

    The LOFT payload module will host two instruments: the Large Area Detector (LAD) and the Wide Field Monitor (WFM).

    LOFT spacecraft (concept design) Credit: LOFT proposal team

    The LAD will improve upon the effective area of the largest area X-ray instrument ever flown (the Rossi X-ray Timing Explorer's Proportional Counter Array) by a factor of about 20. The improved energy resolution (better than 260 eV) of the LAD will allow the exploitation of spectral diagnostics of relativistically-broadened 6-7 keV (Fe-K) lines, in particular. It will be deployed through a mechanism based on that used for Synthetic Aperture Radar missions, such as the Soil Moisture and Ocean Salinity (SMOS) mission, where very large panels are deployed in space with high accuracy.

    The Wide Field Monitor (WFM) will discover and localise X-ray transients and impulsive events and monitor spectral state changes with unprecedented sensitivity. Targeted follow-up observations will make this resource important in its own right.

     

    Instrument specifications

    Parameter

    Requirement

    Goal

    LAD

    Energy range

    2-30 keV (nominal)

    1-40 keV (nominal)

     

    2-50 keV (expanded)

    1-60 keV (expanded)

    Effective area

    10 m²  (2-10 keV)

    12 m²  (2-10 keV)

     

    1.3 m²  (@30 keV)

    2.5 m²  (@30 keV)

     

    <260 eV FWHM (40% of events)

    <200 eV FWHM (40% of events)

    Field of view

    <60 arcmin

    <45 arcmin

    Time resolution

    10 µs

    5 µs

    Dead time

    <0.5% @ 1 Crab

    <0.1% @ 1 Crab

    Background

    <10 mCrab

    <5 mCrab

    Maximum source flux

    >300 mCrab (steady)

    10 Crab (steady)

     

    >15 Crab (peak)

    >30 Crab (peak)

    WFM

    Energy range

    2-50 keV

    1-50 keV

    Energy resolution

    <500 eV FWHM

    <300 eV FWHM

    Field of view

    >3 steradians

    >4 steradians

    Angular resolution

    5 arcmin

    3 arcmin

    Point source localization

    1 arcmin

    0.5 arcmin

    Sensitivity (5σ, 50 ks)

    2 mCrab

    1 mCrab

    Sensitivity (5σ, 1 s)

    0.5 Crab

    0.2 Crab

     

    (Left) A single WFM coded mask module, and (right) an arrangement of several units to cover 3 steradians. Credit: LOFT proposal team.

    The LOFT LAD must cover a geometric area of ~20 m² yet have a reasonably low weight. Large-area Silicon Drift Detectors (SDDs) designed on the heritage of the ALICE experiment at CERN/LHC, and a collimator based on lead-glass microcapillary plates (the mechanical structure of the well-known microchannel plate) would be suitable for a sensitive but light-weight experiment. The detector drift concept makes the spectroscopic performance of the SDDs weakly dependent on the extent of the collecting surface: large-area (~70 cm²) monolithic detectors can be designed, with only 256 read-out anodes (thus low power requirements, ~60 W/m²) but very good spectral performance (FWHM ~260 eV). An unprecedentedly large throughput (~3 x 105 counts per second from the Crab) is achieved with a segmented detector, reducing the impact of pile-up and dead-time, which often limit traditionally focused telescopes.

     

     

    The electrical structure (left) and working principle (right) of a silicon drift detector (SDD). These detectors will be used for the instruments carried on LOFT. Credit: LOFT proposal team

    Left: A micrograph of microchannel plate collimator (MCP) structure; Right: Slump of MCP to achieve the bst source collimation. Credit: LOFT proposal team

     


    Last Update: 21 Mar 2013

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    • Images and Videos
    • LOFT spacecraft concept
    • LOFT wide field monitor
    • Silicon drift detector - electrical structure
    • Silicon drift detector - working principle
    • Microchannel plate collimator

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