Blackwater

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Might get to a pull request, but the algorithm is this: 1. Create a flight trajectory coplanar with the current orbit. 2. When the true anomaly from intercept would be...

My suggestion for defaulting the origin is whatever SOI the current spacecraft is in. So, if you are in orbit around Duna, the default is Duna.

Can you elaborate a little more on that? Do you have references for the math on this?

OK, I've read Braeunig's site more carefully. I wouldn't mind helping on this. Mathwise, I think the only thing that changes is the part where ejection values are calculated in...

Maybe version 1 is only offering the option if eccentricity and inclination is low enough? Then v2 is creating the Hohmann nodes to circularize first. Then V3 is any arbitrary...

If you specify a min/max length of stay, maybe you can just show delta-v versus return-to-start date?

Also may wAnt to include costs of setting inclination of destination parking orbit.