• DocumentCode
    1878570
  • Title

    Radiation Belt Storm Probe spacecraft and impact of environment on spacecraft design

  • Author

    Kirby, Karen ; Bushman, Stewart ; Butler, Mike ; Conde, Rich ; Fretz, Kris ; Herrmann, Carl ; Hill, Adrian ; Maurer, Richard ; Nichols, Richard ; Ottman, Geff ; Reid, Mark ; Rogers, Gabe ; Srinivasan, Dipak ; Troll, John ; Williams, Bruce

  • Author_Institution
    Johns Hopkins Univ. Appl. Phys. Lab., Laurel, MD, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    20
  • Abstract
    NASA´s Radiation Belt Storm Probe (RBSP) is an Earth-orbiting mission scheduled to launch in September 2012 and is the next science mission in NASA´s Living with a Star Program. The RBSP mission will investigate, characterize and understand the physical dynamics of the radiation belts, and the influence of the sun on the earth´s environment, by measuring particles, electric and magnetic fields and waves that comprise the geospace. The mission is composed of two identically instrumented spinning spacecraft in an elliptical orbit around earth from 600 km perigee to 30,000 km apogee at 10 degree inclination to provide full sampling of the Van Allen radiation belts. The twin spacecraft will follow slightly different orbits and will lap each other 4 times per year; this offers simultaneous measurements over a range of spacecraft separation distances. A description of the spacecraft environment is provided along with spacecraft and subsystem key characteristics and accommodations that protect sensitive spacecraft electronics and support operations in the harsh radiation belt environment.
  • Keywords
    radiation belts; space vehicles; Earth-orbiting mission; NASA radiation belt storm probe; RBSP mission; Star Program; Sun; Van Allen radiation belts; earth environment; elliptical orbit; harsh radiation belt environment; particle electric field measurement; particle magnetic field measurement; radiation belt physical dynamics; radiation belt storm probe spacecraft; sensitive spacecraft electronics; spacecraft design; spacecraft environment; spacecraft separation distances; subsystem key characteristics; Belts; Extraterrestrial measurements; Instruments; Plugs; Protons; Space vehicles; Sun; radiation belt; space environment; spacecraft;
  • 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.2012.6187020
  • Filename
    6187020