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I just have a couple of dynamical questions that I'm pondering over:-
If we wanted to maximise the delta-V increments from each successive gravity assist flybys in turn via the 4 giant planets Jupiter, Saturn, Uranus & Neptune (much like Voyager 2's grand tour), what is the maximum (theoretical) final Sun-relative solar system escape velocity that a hypothetical interstellar probe could achieve, and what are the dynamical considerations in such a case? I know Voyager 1 is presently escaping the solar system at 3.6 AUs/year and Voyager 2 at around 3.3 AUs/year, though maximising final escape velocities for these crafts was never a goal in their primary missions of planetary encounter, but supposing it was : what are the theoretical maximums we could achieve by accumulating delta-V gains following each gravity assisted boost via the 4 giant planets in the case of the two Voyagers? On a hypothetical scenario, if we have a *manned* spacecraft of mass 5 x 10^6 kg with an initial approach speed of say 10 km/s plunging into the gravity field of Jupiter on an optimum gravity assisted speed-gaining trajectory , what is the theoretical maximum delta-V that could be gained post-fly by? With the new higher, gravity assisted boost, if this optimum speed-gaining exercise was then repeated at Saturn, Uranus and Neptune, in turn (assuming a favourable positional line up of those planets in their respective orbits) would the cumulative final speed be sufficient for interstellar flight?! Cheers Abdul Ahad |
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