How does SpaceX's Dragon capsule get to the ISS? Does Dragon use the onboard Draco thrusters in order to raise its orbit to the station or does the second stage of the Falcon 9 perform the majority of necessary inclination, altitude, and speed changes?
I’ve heard the Soyuz spacecraft uses its onboard main engine to perform the transfers to the ISS but I don’t see an equivalent to this on board the Dragon.
(Side question: will this procedure change much with Dragon V2?)