1. FIRE - Flyby of Io with Repeat Encounters: A conceptual design for a New Frontiers mission to Io
- Author
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Ross W. K. Potter, John Cumbers, Jason Reimuller, Charles Parker, Morgan L. Cable, L. Lowes, Tanya N. Harrison, Terry-Ann Suer, Shantanu P. Naidu, Charles Budney, Sebastiano Padovan, Jamey Szalay, Jennifer L. Whitten, Catherine C Walker, Diana Gentry, S. Shkolyar, and Harold J. Trammell
- Subjects
Atmospheric Science ,Solar System ,010504 meteorology & atmospheric sciences ,Aerospace Engineering ,Magnetosphere ,Venus ,Io ,01 natural sciences ,Article ,Jovian ,Astrobiology ,Conceptual design ,0103 physical sciences ,010303 astronomy & astrophysics ,0105 earth and related environmental sciences ,Radio Science ,Spacecraft ,biology ,business.industry ,Astronomy and Astrophysics ,space missions ,biology.organism_classification ,Geophysics ,Planetary science ,Space and Planetary Science ,General Earth and Planetary Sciences ,Environmental science ,business - Abstract
A conceptual design is presented for a low complexity, heritage-based flyby mission to Io, Jupiter’s innermost Galilean satellite and the most volcanically active body in the Solar System. The design addresses the 2011 Decadal Surveys recommendation for a New Frontiers class mission to Io and is based upon the result of the June 2012 NASA-JPL Planetary Science Summer School. A science payload is proposed to investigate the link between the structure of Io’s interior, it’s volcanic activity, it’s surface composition, and it’s tectonics. A study of Io’s atmospheric processes and Io’s role in the Jovian magnetosphere is also planned. The instrument suite includes a visible/near IR imager, a magnetic field and plasma suite, a dust analyzer and a gimbaled high gain antenna to perform radio science investigations. Payload activity and spacecraft operations would be powered by three Advanced Stirling Radioisotope Generators (ASRG). The primary mission includes 10 flybys with close-encounter altitudes as low as 100 km. The mission risks are mitigated by ensuring that relevant components are radiation tolerant and by using redundancy and flight-proven parts in the design. The spacecraft would be launched on an Atlas V rocket with a delta-v of 1.3 km/s. Three gravity assists (Venus, Earth, Earth) would be used to reach the Jupiter system in a 6-year cruise. The resulting concept demonstrates the rich scientific return of a flyby mission to Io.
- Published
- 2017
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