Has SpaceX provided any details on their specific plans for the trajectory of the Falcon Heavy payload propulsion on its trip out as far as Mars orbit? I'm wondering if they have made public whether they are launching directly towards Mars orbit or if they will orbit the earth for a few rotations first.
Also, will the 2nd stage Merlin Vacuum engine provide all of the thrust necessary to get to Earth orbit and then use the same engine to get out of Earth's gravity towards Mars orbit? I know the Merlin Vacuum engine can be re-fired multiple times, but I do not know if getting to earth orbit, then getting out of Earth's gravity field will run the motor significantly longer than it's ever run before on a flight.