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Solar-Powered Europa Orbiter Design Study (2007)The feasibility of implementing a solar-powered mission around Europa has been evaluated periodically over the last decade. Most recently, an assessment was performed as part of the 2006 Europa Explorer (EE) Study, which evaluated the practicality of implementing that mission design with large solar arrays instead of radioisotope power systems (RPS). This previous study went into some depth in considering the issues related to the use of solar arrays in the Europa orbit illumination and radiation environment. The study concluded that an all-solar option was impractical to meet the science objectives as defined in that study by the science team. This conclusion resulted from the prohibitive mass, packaging and articulation issues associated with the very large (approx.300 sq m) solar arrays required to accommodate frequent eclipse periods associated with the particular Europa orbit used.
Document ID
20080015542
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Elliott, John
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Langmaier, Jerry
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pappalardo, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Strange, Nathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Spilker, Tom
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lock, Rob
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Reh, Kim
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JPL 08-02
Distribution Limits
Public
Copyright
Other
Keywords
Europa
Europa Explorer
solar powered missions
solar arrays

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