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