Quote:
Originally Posted by PTTG
You want the sum of the ΔV required to break orbit from the origin, the ΔV used in the transfer itself, and then, yes, the ΔV expended to attain orbit at the destination.
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Just to be exhaustive there's the possibility of an change or orbital plane maneuver. It was part of the effect of launching from Cape Canaveral for the Moon that on the right days no change of plane was needed.
It's usually a glossed over effect and I know of no easy databases but the planets of our solar system mostly do have different orbital planes..