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    Fact Sheet

    Fact Sheet: Double Star Programme - a joint project between ESA and the China National Space Administration
      Double Star Programme - a joint project between ESA and the China National Space Administration
    Double Star follows in the footsteps of ESA's ground-breaking Cluster mission by studying the effects of the Sun on the Earth's environment. Conducting joint studies with Cluster and Double Star increases the overall scientific return from both missions.

    Mission Objectives

    Double Star is the first mission launched by China to explore the Earth's magnetosphere - the magnetic bubble that surrounds our planet.

    Mission Name

    As its name suggests, Double Star involves two satellites - each designed, developed, launched, and operated by the China National Space Administration (CNSA). The two spacecraft are called TC-1 and TC-2, where TC stands for 'Tan Ce' which means 'Explorer'.

    Spacecraft

    Each DSP spacecraft is cylindrical with a 1400 mm height and 2100 mm diameter and is spin-stabilised at 15 rpm. The height of the body-mounted solar array is 740 mm. The configuration of the spacecraft is with two 2.5 m experimental rigid booms and two axial telecommunication antenna booms.

    Instruments

    Equatorial Double Star

    Instruments

    PI

    Active Spacecraft Potential Control (ASPOC) K. Torkar
    IWF
    Graz
    Austria
    Fluxgate Magnetometer (FGM) C. Carr
    IC
    United Kingdom
    Plasma Electron and Current Experiment (PEACE) A. Fazakerley
    MSSL
    Dorking
    United Kingdom
    Hot Ion Analyzer (HIA), sensor 2 of CIS H. Rème
    CESR
    Toulouse
    France
    Part of Spatio-Temporal Analysis of Field Fluctuations (STAFF) + Digital Wave Processor (DWP) N. Cornilleau & H. Alleyne
    CETP
    Vélizy, France
    Sheffield University, United Kingdom
    High Energy Electron Detector (HEED) * W. Zhang and J.B. Cao
    CSSAR
    China
    High Energy Proton Detector (HEPD) * J. Liang and J.B. Cao
    CSSAR
    China
    Heavy Ion detector (HID) * Y. Zhai and J.B. Cao
    CSSAR
    China

    Polar Double Star

    Instruments

    PI

    Neutral Atom Imager (NUADU) S.McKenna-Lawlor
    STI Ltd.
    National University of Ireland
    Co. Kildare
    Ireland
    Fluxgate Magnetometer (FGM) T. Zhang
    IWF
    Austria
    Plasma Electron and Current Experiment (PEACE) A. Fazakerley
    MSSL
    Dorking
    United Kingdom
    Low Energy Ion Detector (LEID) * Q. Ren and J.B. Cao
    CSSAR
    China
    Low Frequency Electromagnetic Wave Detector (LFEW) * Z. Wang and J.B. Cao
    CSSAR
    China
    High Energy Electron Detector (HEED) * W. Zhang and J.B. Cao
    CSSAR
    China
    High Energy Proton Detector (HEPD) * J. Liang and J.B. Cao
    CSSAR
    China
    Heavy Ion Detector (HID) * Y. Zhai and J.B. Cao
    CSSAR
    China

    (* Instrument originated in China)

    Orbit

    The Equatorial spacecraft (TC-1) was launched into an elliptical orbit of 570 x 78 970 kilometres, inclined at 28.5° to the equator on 29 December 2003. This enables it to investigate the Earth's huge magnetic tail, the region where particles are accelerated towards the planet's magnetic poles by a process known as reconnection. TC-1's nominal period of operations is expected to be 18 months.

    The Polar satellite (TC-2) was launched 25 July 2004 into a polar orbit of 700 x 39 000 kilometres. Its instruments will concentrate on the physical processes taking place over the magnetic poles and the development of auroras. It is expected to operate for at least one year.

    Operations Centre

    Data is relayed to the ESA ground station at Villafranca, Spain, and the Chinese ground stations in Beijing and Shanghai, China.


    Last Update: 15 Nov 2010

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