Salamander
Orbinaut
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how about making the transfer ejection burn prograde, then add a pane alignment burn later on when the relative velocity is much lower?
the total flight time might be a bit longer then (because it involves a slight detour), but the delta V requirement would be much lower.
the total flight time might be a bit longer then (because it involves a slight detour), but the delta V requirement would be much lower.
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