Thanks Atuhalpa.
BTW I just managed to find a solution to an enhanced grand tour. It's a voyager outer planet finish but starts several years earlier with inner planet slings so it visits ALL planets. It has an almost identical initial transfer burn as the Voyager missions, which is pretty energetic considering it's only heading to Venus but it does the trick.
In planning it, after several inner slings TransX was becoming unstable so I did a little trick that's sometimes needed... the Cl App was wandering around at the 41696 Venus encounter (see data below) leaving me unable to adjust slings after that encounter, so when it was close I looked at the date and encounter velocity and then turned off inherit velocity and entered the date and velocity manually.
Then it stabilized and allowed continuing sling planning to what ultimately was a 25 stage flightplan. Data is as follows...
Depart Earth Jan 16, 1968, MJD=39871.6808, Pro=-7.903Km, Out=-3.887Km, PlaneCh=-714.5m
Slings with MJD dates are as follows...
Venus 40000
Mercury 40212
Mercury 40476
Venus 41349
Mars 41522
Venus 41696
Venus 42237
Earth 43297
Jupiter 44126
Saturn 44952
Uranus 46687
Neptune 48097
...
The reason I searched this sling cascade is that this thread is about real world sims and using a craft that supposed to be limited to current day technology. Yes this flight is an after the fact "what if" but it's not unreasonable to say "what if the voyager planetary alignment concept had been noticed earlier" and was set up to include an inner planet enhancement of which this is just an example. In any event it would surely be a challenge to fly this mission no matter what craft you use. The goal would be to limit the total MCC corrections to a minimum because there are probably going to be quite a few with 12 slings on the menu. To sim real life it would just need a craft that can handle 22 years of exposure to the space environment. Since the Voyager is still with a pulse (i think) I suppose that's within real life too.
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I just flew the enhanced Voyager mission and have some observations to make. The dates mentioned above are fairly accurate with regard to the inner planets but it actually came closer to the real Voyager mission than predicted for the outer planets. The arrival dates at each planet are as follows...
Venus 40000 (as predicted)
Mercury 40212 (as predicted)
Mercury 40476 (as predicted)
Venus 41349 (as predicted)
Mars 41518 (4 days ahead of plan)
Venus 41696 (as predicted)
Venus 42237 (as predicted)
Earth 43297 (as predicted)
Jupiter 44046 (in between the two Voyager missions)
Saturn 44952 (in between the two Voyager missions)
Uranus 46416 (6 weeks ahead of the Voyager mission)
Neptune 47715 (3 weeks ahead of the Voyager mission)
The mission was completely free coasting with no deep space maneuvers but there were on average something like 25 m/s per sling corrections for the inner planets and about 55 m/s per sling for the outer planet planet slings. The total dv used for all slings from the initial transfer from Earth to passing Neptune was 405 m/s. Not bad for 12 slings in all. The initial transfer burn was 6336 m/s from LEO.