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    Instruments

    Instruments In Brief

    The Planck scientific instrument complement comprises two instruments, LFI, a radio receiver array covering the lower frequency range, and HFI, a bolometric detector array covering the higher frequencies. The instruments share a common telescope. Principal Investigator (PI) consortia provide the instruments and telescope. 

    Planck Principal Investigators

    LFI

    Nazzareno  Mandolesi, Istituto di Tecnologie e Studio delle Radiazioni Extraterrestri, (Bologna, Italy). Deputy PI: Marco Bersanelli, Universita' degli Studi di Milano (Milan, Italy)

    HFI

    Jean-Loup Puget, Institut d'Astrophysique Spatiale,  (Orsay, France). Deputy PI: François Bouchet, Institut d'Astrophysique de Paris (Paris, France)

    Telescope

    Hans-Ulrik Norgaard Nielsen, Danish Space Research Institute, (Copenhagen, Denmark)


    Low Frequency Instrument

    The Low Frequency Instrument (LFI) is designed to produce high-sensitivity, multi-frequency measurements of the microwave sky in the frequency range 27 to 77 GHz (wavelength range 11.1 to 3.9 mm).

    LFI Performance Goals

    Centre frequency (GHz)

    30

    44

    70

    Bandwidth (GHz)

    6

    8.8

    14

    Beamwidth (arcminutes, FWHM)

    33

    24

    14

    Detector technology

    High electron mobility transistor (HEMT) radio receiver arrays

    Detector temperature (K)

    ~ 20

    Cooling technology

    H2 sorption cooler

    Average ΔT/T1 per pixel*

    2

    2.7

    4.7

    Average ΔT/T2 per pixel*

    2.8

    3.9

    6.7

    Flux sensitivity per pixel* (mJy)

    13

    19

    25

     

    * A pixel is a square whose side is the full width, half maximum (FWHM) extent of the beam. These sensitivity figures are calculated for the average integration time per pixel. The integration time will be very inhomogeneously distributed over the sky and will be much higher in certain regions.

    1Sensitivity (1 σ) to intensity (Stokes I) fluctuations, measured in thermodynamic temperature units × 10-6, relative to the average temperature of the CMB (2.73 K), achievable after two sky surveys (14 months).

    2Sensitivity (1 σ) to polarised intensity (Stokes U and Q) fluctuations, measured in thermodynamic temperature units × 10-6, relative to the average temperature of the CMB (2.73 K), achievable after two sky surveys (14 months).


    High Frequency Instrument

    The High Frequency Instrument (HFI) is designed to produce high-sensitivity, multi-frequency measurements of the diffuse sky radiation in the frequency range 84 GHz to 1 THz (wavelength range 3.6 to 0.3 mm).

    HFI Performance Goals

    Centre frequency (GHz)

    100

    143

    217

    353

    545

    857

    Bandwidth (GHz)

    33

    47

    72

    116

    180

    283

    Beamwidth (arcminutes, FWHM)

    9.2

    7.1

    5

    5

    5

    5

    Detector technology

    Spider bolometer arrays,
    neutron transmutation doped (NTD) germanium thermistors

    Detector
    temperature (K)

    ~ 0.1

    Cooling technology

    H2 sorption cooler + Joule-Thomson cooler + 3He/4He dilution cooler

    Average ΔT/T3
    per pixel*

    2

    2.2

    4.8

    14.7

    147

    6700

    Average ΔT/T4
    per pixel*

     

    4.2

    9.8

    29.8

     

     

    Flux sensitivity
    per pixel* (mJy)

    9

    12.6

    9.4

    20

    46

    52

     

    * A pixel is a square whose side is the full width, half maximum (FWHM) extent of the beam. These sensitivity figures are calculated for the average integration time per pixel. The integration time will be very inhomogeneously distributed over the sky and will be much higher in certain regions.

    3Sensitivity (1 σ) to intensity (Stokes I) fluctuations, measured in thermodynamic temperature units × 10-6, relative to the average temperature of the CMB (2.73 K), achievable after two sky surveys (14 months).

    4Sensitivity (1 σ) to polarised intensity (Stokes U and Q) fluctuations, measured in thermodynamic temperature units × 10-6, relative to the average temperature of the CMB (2.73 K), achievable after two sky surveys (14 months).


    Measurement Results

    The measurements made by the two instruments will be combined and used to produce a full-sky map of the anisotropies in the Cosmic Microwave Background (CMB) with unprecedented precision. This map will in turn be used to derive a wealth of cosmological information, including an accurate determination of the values of the main parameters that characterise the large-scale structure and evolution of the Universe.

    Telescope

    The telescope design is an off-axis tilted Gregorian system, offering the advantages of no blocking of the optical path combined with compactness. The eccentricity and tilt angle of the secondary mirror and the off-axis angle obey the Dragone-Mizuguchi condition, which allows the system to operate without significant degradation over a large focal plane array, while simultaneously minimizing the polarization effects introduced by the telescope.

    The baffling system is composed of two elements. The shield element is a large, self-supporting and roughly conical structure covered with multi-layer insulation (MLI), which surrounds the telescope and focal plane instruments. Together with the optical bench, it defines the optical enclosure. It has two important functions, reducing the level of straylight (which at the chosen orbit is in large part due to the spacecraft itself) and promoting the radiative cooling of the optical enclosure towards deep space. The baffle element consists of one half of a conically shaped surface that links the focal plane instruments to the bottom edge of the sub-reflector. The function of the baffle is to shield the detectors from thermal radiation originating within the optical enclosure. 

    Telescope characteristics
    Type

    Off-axis tilted Gregorian

    Primary mirror

    1.9 × 1.5 m, off-axis paraboloid

    Secondary mirror

    1.1 × 1.0 m, off-axis paraboloid

     

    Introduction

    Last Update: 11 Jul 2012

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