Elroch, no problem, your posts made me think and that's always good. (Though perhaps not all who know me would agree.

)
However, I still have a question I would like to pose, even though it may mess things up again.

Consider the three observers on the Earth that we've been discussing (by "Earth" I mean the idealized, exactly oblate spheroidal Earth with the frictionless ocean surface that is *exactly* an equipotential surface in terms of "rate of time flow"). Observer A is at the North Pole. Observer B is at the equator and got there by sliding slowly Southward, with zero energy change, from the North Pole; by my earlier argument, he is therefore still at rest in an inertial frame (not rotating with the Earth), so he is moving at 1000 mph westward relative to Observer C, who is at the equator and rotating with the Earth.
Here's the question: for each of these observers, how much energy would a rocket need to expend to launch them into a marginal escape trajectory, i.e., a trajectory that just barely escapes "to infinity" from the Earth's gravity? (Assume no other bodies in the universe.) I'm not so much interested in exact numbers as in the relationship between the numbers for A, B, and C.
Thoughts?