EUROPA Multiple-Flyby Trajectory Design

Buffington, Brent; Campagnola, Stefano; Petropoulos, Anastassios

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NASA NTRS · 20130003153

EUROPA Multiple-Flyby Trajectory Design

Buffington, Brent·Campagnola, Stefano·Petropoulos, Anastassios

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Abstract

As reinforced by the 2011 NRC Decadal Survey, Europa remains one of the most scientifically intriguing targets in planetary science due to its potential suitability for life. However, based on JEO cost estimates and current budgetary constraints, the Decadal Survey recommended-and later directed by NASA Headquarters-a more affordable pathway to Europa exploration be derived. In response, a flyby-only proof-of-concept trajectory has been developed to investigate Europa. The trajectory, enabled by employing a novel combination of new mission design techniques, successfully fulfills a set of Science Definition Team derived scientific objectives carried out by a notional payload including ice penetrating radar, topographic imaging, and short wavelength infrared observations, and ion neutral mass spectrometry in-situ measurements. The current baseline trajectory, referred to as 11-F5, consists of 34 Europa and 9 Ganymede flybys executed over the course of 2.4 years, reached a maximum inclination of 15 degrees, has a deterministic delta v of 157 m/s (post-PJR), and has a total ionizing dose of 2.06 Mrad (Si behind 100 mil Al, spherical shell). The 11-F5 trajectory and more generally speaking, flyby-only trajectories-exhibit a number of potential advantages over an Europa orbiter mission.

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Buffington, Brent, Campagnola, Stefano, Petropoulos, Anastassios. 2012-08-13. EUROPA Multiple-Flyby Trajectory Design. https://ntrs.nasa.gov/citations/20130003153

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