PAllen said:
I assume we can kick each whatever direction we want to escape to infinity in any desired path. In particular, there is an obvious better kick direction for C.
Yes, an object can achieve escape velocity in any direction (even *towards* the gravitating body, as long as it doesn't actually hit it--i.e., a close grazing approach), and still escape. So the obvious way to get C to escape is to boost it in the direction it's already moving because of the Earth's rotation.
PAllen said:
Now I am a little queasy that these are not correlated to the time flow rates. Yet I find any other conclusion hard to accept.
That's why I posed the question.

I felt queasy too until I thought about it some more. See below.
Elroch said:
My immediate thought is that this consideration should have told me that someone co-rotating at the equator has a different energy to one stationary at the pole! When launching rockets into orbit, less energy is required if you start near the equator (C). If I recall, even Jules Verne took account of this in "from the Earth to the moon", and it is taken advantage of by the US launch sites, amongst others.
Yes.
Elroch said:
The other two sites (A and B) require the same energy if they are at the same gravitational potential but are stationary w.r.t. the centre of the Earth.
But *are* they at the same "gravitational potential"? That's the question.
PAllen said:
Moving from state A to state B requires some work against gravity. The result is time for B runs faster than A. To get from B state to C state, you have to do more work to add KE (1000 mph in polar inertial frame). However, this KE, leaving potential unchanged, but adding velocity, makes time slow down.
Note, I always insisted that the earth, including the sea, was oblate due to rotation. I said this a number of times, arguing that if you got to the equator on a frictionless surface just above the sea, time would be slower than at the pole. I may not have always been clear about the implication that this implies significant work is needed to get from the pole to the equator even on a frictionless surface.
The Earth is certainly oblate due to rotation. That's been known for a long time:
http://en.wikipedia.org/wiki/Figure_of_the_Earth
The equation for "gravitational potential", according to GR, is, approximately, this:
\frac{d \tau}{dt} = \sqrt{1 - \frac{2 G M}{c^{2} r} - \frac{v^{2}}{c^{2}}}
where I have included explicit factors of G and c, contrary to my usual practice.
I say "approximately" because there are at least two types of corrections that could be applied. One is that the Earth is not a perfect oblate spheroid, so there is a correction to the M/r term. It's been a while since I computed it, but IIRC it's small compared to the base correction expressed above. The other is that the Earth is rotating, so the spacetime metric around it is not perfectly Schwarzschild, which is what the above equation assumes; it's actually slightly Kerr, meaning there is an extra term for "frame dragging" due to the Earth's angular momentum. IIRC this term is way smaller than the others, so we can ignore it here.
Since the Earth itself is rotating, the shape of its surface (in the idealized case we've been considering) is determined by balancing v vs. r at every point to keep d \tau / dt constant. So the Earth's surface is equipotential, as Elroch said. But since "equipotential" includes the effects of v, if you are on the Earth's surface but your v differs from the local v of the surface at that point, your potential will *not* be the same as that of the Earth's surface at that point. So observer B *is* at a higher *potential* than observer A, as PAllen said; it *will* take work against gravity to move from A to B, even if the Earth's surface is frictionless.
So I agree with PAllen's answer here:
PAllen said:
Next large kick needed for B, and most for A.
Since it takes work against gravity to move from A to B, that work can be subtracted from the rocket energy required to launch from B, so more energy is required for A than B. And since C has extra kinetic energy compared to B, but is at the same height, it takes less energy to launch C than B, as everyone seems to agree. So the full ordering is C < B < A.
Now, what about time flow rates? We have C < B < A for launch energy, but C = A < B for time flow rate. That's because the intuitive guess that potential energy, in the sense of "height", should be the same as time flow rate only holds for observers that are *static* in the field. A and B are static, but C is not. (Note that "static" means "not rotating with the Earth", because "static" is determined by the time translation symmetry of the spacetime as a whole, i.e., of the metric.) So we can directly relate the difference in time flow rate between A and B to the difference in their heights. But C is moving, so his time flow rate is a combination of two effects (as shown in the equation I gave above), his height and his velocity; and because the Earth's surface is equipotential, the slowdown due to his velocity is just right to offset the speedup due to his height, when compared with A. But compared to B, he's at the same height, so the only difference is his velocity, hence C is slower than B (and by the *same* amount as A, of course).