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6

Yes, but really no. Preamble: I built a little 2D trajectory simulation (2D because the Galilean moons are more or less coplanar) to test out trajectories (Jupiter + Galilean moons gravity, RK4, 10s time step). My original intention was to perform an exhaustive search across 4 dimensions of initial conditions but this was prohibitively expensive (...


2

Edit: re-reading the question this is not an answer, which is looking for solutions involving gravity assists only while this only covers aerobraking orbit adjustment The study here (summary is section 6.4) found that for an example mission profile while substantial mass/cost savings would be possible it would involve several years of orbital shaping to ...


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