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
Link To Document :
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