• DocumentCode
    1878407
  • Title

    Juno radiation design and implementation

  • Author

    Kayali, Sammy ; McAlpine, William ; Becker, Heidi ; Scheick, Leif

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    Juno, the second NASA New Frontiers mission, was launched to Jupiter on August 5, 2011 from Cape Canaveral Air Station onboard an Atlas V launch vehicle. The mission features a solar powered, spinning spacecraft in a highly elliptical polar orbit that avoids much of Jupiter´s highest radiation regions. Developing and operating a spacecraft in the environment of space can be a technical and a programmatic challenge and the Juno Mission has the added challenge of operating in the severe radiation environment of Jupiter. This paper describes the Juno Mission and the preparations, which were required to develop and implement a mission, and spacecraft design to successfully operate in the harsh Jovian environment and provide the desired science returns.
  • Keywords
    space research; space vehicles; Atlas V launch vehicle; Cape Canaveral Air Station onboard; Juno Mission; Juno radiation design; Jupiter; NASA New Frontiers mission; harsh Jovian environment; programmatic challenge; Aircraft manufacture; Instruments; Jupiter; Materials; Orbits; Space vehicles; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187013
  • Filename
    6187013