• DocumentCode
    469470
  • Title

    The electronic ground support equipment for the silicon tracker cooling system of the AMS-02 experiment

  • Author

    Accardo, Lucio ; Alberti, Gabriele ; Bardet, Michiel ; Battiston, Roberto ; Blasko, Sandor ; He, Zhenghui ; Jiang, Xiao Hua ; Koutsenko, Vladimir ; Lebedev, Alexei ; Menichelli, Mauro ; Ni, Jiangqun ; Papi, Andrea ; Van Es, J. ; Tang, Chengpei ; Wang, Zix

  • Author_Institution
    Ist. Nazionale di Fisica Nucl., Perugia
  • Volume
    1
  • fYear
    2007
  • fDate
    Oct. 26 2007-Nov. 3 2007
  • Firstpage
    411
  • Lastpage
    415
  • Abstract
    AMS-02 is a space experiment that will perform cosmic ray studies on board of the international space station starting from July 2009. This paper describes the design and production of electronic ground support equipment (EGSE) that emulates the silicon tracker cooling system in the AMS-02 apparatus. This emulator is needed in order to test the control electronics of the cooling system without the cooling system itself. The cooling system will be assembled and integrated separately and with a different schedule. Using the EGSE, with a proper emulation software, it will also be possible to simulate the behavior of the cooling system in space. The tracker cooling system includes a set of different sensors and actuators which are necessary for bringing the tracker detector to a uniform temperature at which it can operate properly. The sensors include: Pt1000 thermistors, semiconductor thermal sensors, differential and absolute pressure sensors, and pump rotational speed sensors. The actuators are: resistive heaters, Peltier heat pumps and liquid pumps. The EGSE should simulate the behavior of all these sensors and actuators. This means that it must generate the same signals from the electrical point of view but also its global behavior, namely the response to any internal and external condition change should be the same as the actual tracker cooling system. In order to achieve this performance appropriate software that includes the simulated response of the tracker cooling system will be developed. The EGSE has been developed in three phases: in phase 1 we emulated the electrical behavior of each sensor or actuator as a single unit, in phase 2 we integrated those sensors in a single unit and we added a USB computer interface and basic control software. In phase 3 we will develop software emulating the behaviour of the entire tracker cooling system.
  • Keywords
    computer interfaces; high energy physics instrumentation computing; nuclear electronics; particle tracks; silicon radiation detectors; thermistors; AMS-02 experiment; Peltier heat pumps; Pt1000 thermistors; USB computer interface; actuators; control electronics; control software; cosmic ray; differential pressure sensors; electronic ground support equipment; emulation software; international space station; pump rotational speed sensors; resistive heaters; semiconductor thermal sensors; silicon tracker cooling system; space experiment; tracker cooling system; Actuators; Electronic equipment testing; Electronics cooling; Ground support; Heat pumps; International Space Station; Silicon; Space stations; Temperature sensors; Thermal sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Nuclear Science Symposium Conference Record, 2007. NSS '07. IEEE
  • Conference_Location
    Honolulu, HI
  • ISSN
    1095-7863
  • Print_ISBN
    978-1-4244-0922-8
  • Electronic_ISBN
    1095-7863
  • Type

    conf

  • DOI
    10.1109/NSSMIC.2007.4436359
  • Filename
    4436359