• DocumentCode
    3162312
  • Title

    Star tracker design considerations for the Europa Orbiter mission

  • Author

    Liebe, Carl Christian ; Eisenman, Allan R. ; Hancock, Bruce R. ; Mellstrom, Jeffrey A. ; Ratliff, J. Martin ; Swift, Gary M. ; Alexander, James W. ; Wadsworth, Mark ; Walker, W. John

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    67
  • Abstract
    Star trackers are an accurate device used by most spacecraft to autonomously determine their orientation. The future Europa Orbiter mission poses significant environmental challenges not typically encountered in other space missions. The Jovian system in which the star tracker must operate is characterized by extremely intense ionizing radiation, which is primarily due to high-energy electrons and protons trapped by Jupiter´s magnetic field. The design of a star tracker that will operate in this environment must overcome many challenging problems. Ionizing radiation will cause ordinary optical glass to darken. Silicon based detectors typically experience threshold shifts, increased dark current, reduced quantum efficiency and reduced charge transfer efficiency (in the case of CCDs). An even larger challenge is posed by the charged particle flux impinging on the detector. Charged particles incident on any glass in the optical path will generate luminescence and Cerenkov radiation, which degrades the signal to noise ratio. This paper discusses issues related to the design of a star tracker that can operate in the Europa radiation environment
  • Keywords
    CCD image sensors; Cherenkov radiation; Jupiter; aerospace instrumentation; elemental semiconductors; optical glass; planetary magnetism; planetary satellites; radiation hardening (electronics); shielding; silicon; space research; space vehicles; CCD; Cherenkov radiation; Europa orbiter mission; Jovian system; Si; Si detectors; Star tracker design; charge transfer efficiency; charged particle flux impinging; dark current; environmental challenges; high-energy electrons; high-energy electrons and protons; ionizing radiation; luminescence; optical glass; quantum efficiency; star tracker; threshold shifts; Detectors; Electron traps; Glass; Ionizing radiation; Jupiter; Magnetic fields; Protons; Space missions; Space vehicles; Ultraviolet sources;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1999. Proceedings. 1999 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • Print_ISBN
    0-7803-5425-7
  • Type

    conf

  • DOI
    10.1109/AERO.1999.793147
  • Filename
    793147