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
Link To Document :
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