PeterDonis said:
I'll defer further discussion of that question to a separate post
Here is at least the start of the further discussion.
I figured out just now why I have had the feeling all through this thread that there was something nagging at me that I hadn't gotten out into the open. Let me approach it by recapping pervect's reasoning in the previous thread where he derived his "sliding block" metric, since this will establish fixed points on which we both agree.
We are considering a block sliding along the floor of a rocket that is accelerating. Here I'll continue my coordinate conventions, which are that, in a fixed inertial frame with Minkowski coordinates ##T, X, Y, Z##, the floor of the rocket has proper acceleration ##g## in the ##X## direction, and the block is sliding, relative to the rocket, in the ##Y## direction. We are for now only considering the bottom of the block, i.e., the surface of the block that is in contact with the floor of the rocket. In other words, we are only looking at events on the hyperbolic "worldsheet" defined by ##X^2 - T^2 = 1 / g^2## (but with the ##Y## coordinate unconstrained); note that I am using my convention for this, not pervect's, which shifts the ##X## coordinate by ##1/g## so that the floor of the rocket is at ##X = 0## at ##T = 0##, instead of ##X = 1/g##.
In order to specify the motion of the floor of the block, we have to determine what the constraint is. Pervect's constraint, which I agree with, is that, in the fixed inertial frame, the momentum of the block in the ##Y## direction should be constant. This means the ordinary velocity of the block in the ##Y## direction, in the fixed inertial frame, will decrease with time, for reasons which pervect explained in the previous thread (and which I agree with). Pervect expressed this constraint using a constant ##K = dY / d\tau## (where I have switched to ##Y## instead of x and capitalized it to agree with the coordinate convention I'm using, where capital letters refer to inertial coordinates).
I expressed this constraint somewhat differently. My approach was to observe that, in the momentarily comoving inertial frame of the floor of the rocket, the ordinary velocity of the block in the ##Y'## direction (we'll use a prime for the MCIF to distinguish it from the fixed inertial frame above) will also be constant; I called this constant velocity ##v##. We can easily show that my constraint is equivalent to pervect's constraint. In the MCIF, we have ##\partial T' / \partial \tau = \gamma##, where ##\tau## is the proper time of the block and ##\gamma = 1 / \sqrt{1 - v^2}##, and by the chain rule we have ##\partial Y' / \partial \tau = ( \partial T' / \partial \tau ) \partial Y' / \partial T' = \gamma \partial Y' / \partial T' = \gamma v##. Finally, since ##Y = Y'##, because the MCIF and the fixed inertial frame only differ by a boost in the ##X'## direction, we have ##K = \partial Y / \partial \tau = \partial Y' / \partial \tau = \gamma \partial Y' / \partial T' = \gamma v##. So a constant ##K## implies a constant ##v## and vice versa.
Combining all this gives the 4-velocity of the block, expressed in the Minkowski coordinates of the fixed inertial frame (note that this is somewhat different from the expressions I frequently used before, since I have replaced the ##\cosh## and ##\sinh## functions, which did not have Minkowski coordinates as arguments, with their equivalent functions of Minkowski coordinates, so ##\cosh g \gamma \tau = g X## and ##\sinh g \gamma \tau = g T##):
$$
U = \gamma g X \partial_T + \gamma g T \partial_X + \gamma v \partial_Y
$$
So far we are all in agreement. But now comes the key point, which was nagging at me before. Everything we've done so far only applies to the floor of the rocket, and to the bottom of the block. But pervect and I have both proposed metrics for the "block frame", and those metrics are not restricted to the floor of the rocket and the bottom of the block. They include the ##\chi## direction, which is the direction of proper acceleration, and is orthogonal to the ##\tau \psi## plane that describes the floor of the rocket and the bottom of the block. So we need to make
some sort of assumption about what happens in that direction.
To put the point another way, consider the top surface of the block. It is separated, in the ##X##, ##X'##, or ##\chi## direction, from the bottom surface of the block and the floor of the rocket. What does the motion of this surface of the block look like, to an observer who is at rest relative to the bottom of the block?
For the rocket, we know the answer to this question: the top of the rocket is at a fixed "ruler distance" from the bottom (which is just the difference in their Rindler ##x## coordinates--note that this is
not the same as the difference in their Minkowski ##X## coordinates, which decreases with time), and has less proper acceleration; the latter varies inversely with ##x##. So we can describe the 4-velocity of the top of the rocket just as easily as we can that of the bottom. In Minkowski coordinates, it is
$$
U_{r} = \frac{gX}{g \sqrt{X^2 - T^2}} \partial_T + \frac{gT}{g \sqrt{X^2 - T^2}} \partial_X
$$
I have included the explicit factors of ##g## to make clear the point: we cannot just take the 4-velocity of the floor of the rocket, which would be ##\sqrt{1 + g^2 T^2} \partial_T + g T \partial_X##, and "extend" it to the rest of the rocket and assume that it applies. In order to properly specify the congruence of worldlines that describes the rocket, we must look at the conditions that the congruence must satisfy, and find a 4-velocity field that satisfies those conditions. The 4-velocity ##U_r## that I wrote above does this for the rocket: as is easily verified by computation, the congruence ##U_r## has zero expansion, shear, and vorticity, and its proper acceleration varies with "altitude" (meaning, with ##\sqrt{X^2 - T^2}##, since that is the constant that labels each worldline in the congruence--in Rindler coordinates it is just ##x##), whereas the proper acceleration of the congruence ##\sqrt{1 + g^2 T^2} \partial_T + g T \partial_X## does not--it is always ##g##. (This latter congruence, btw, is easily seen to be the "Bell congruence", which plays a key role in the Bell spaceship paradox, and of course it is known to have nonzero expansion, which is why the string in the Bell spaceship paradox eventually breaks.)
Once we find the 4-velocity field ##U_r## that describes the rocket, we then need only find a coordinate chart in which integral curves of ##U_r## have constant spatial coordinates, i.e., we want a chart ##t, x, y, z## in which ##U_r = \partial_t / | \partial_t |##. This chart will be our desired "rocket frame", a non-inertial frame in which the rocket is at rest. (Of course this chart turns out to be the Rindler chart.) Similarly, once we have found a 4-velocity field ##U_b## that satisfies the conditions for a congruence describing the sliding block, we need only find a chart ##\tau, \chi, \psi, z## in which the integral curves of ##U_b## are given by ##U_b = \partial_{\tau} / | \partial_{\tau} |##, and that will be our desired "block frame", a non-inertial frame in which the block is at rest.
The claim I have been making in this thread can now be stated very simply: the 4-velocity field that I presented in previous posts
is the desired ##U_r##, and the chart I derived in which its integral curves have constant spatial coordinates,
is the desired chart for the "block frame" as described above. The one reservation I had, about the congruence having nonzero shear, I have now resolved; I rechecked my computation of the shear and found that I had made a mistake. The shear is actually zero. The vorticity is still nonzero, but that's OK; we have been in agreement that nonzero vorticity is to be expected (though I think the question of what, exactly, it means physically still deserves some discussion). In the notation I have been using in this post, that 4-velocity field is
$$
U_{b} = \frac{gX}{\sqrt{g^2 \left( X^2 - T^2 \right) - v^2}} \partial_T + \frac{gT}{\sqrt{g^2 \left( X^2 - T^2 \right) - v^2}} \partial_X + \frac{v}{\sqrt{g^2 \left( X^2 - T^2 \right) - v^2}} \partial_Y
$$
Conversely, the implied 4-velocity field pervect has been using, which corresponds to taking the 4-velocity field ##U = \gamma g X \partial_T + \gamma g T \partial_X + \gamma v \partial_Y##, which is valid at the bottom of the block, and extending it over all of the block, does
not work. That should be evident by comparison with the Bell congruence vs. the Rindler congruence above; my 4-velocity field ##U_b## corresponds to ##U_r## above, and pervect's 4-velocity field, which works out to ##U = \gamma \sqrt{1 + g^2 T^2} \partial_T + \gamma g T \partial_X + \gamma v \partial_Y##, corresponds to the Bell congruence ##U = \sqrt{1 + g^2 T^2} \partial_T + g T \partial_X## above. So pervect's chart, in which integral curves of his 4-velocity field ##U## have constant spatial coordinates, corresponds to a "Bell chart" in which integral curves of the Bell congruence have constant spatial coordinates. I predict, therefore, that if we can compute the kinematic decomposition of pervect's congruence, we will find that it has nonzero expansion. In other words, objects at rest in his chart will not remain at a constant proper distance from each other; they will "move apart" with time.
One final note: what about the condition that ##dY / d\tau## must be constant along a given block worldline? The formula for ##U_b## above certainly does not make that evident. However, we can see that it is still true by noting that the denominator of all the terms in ##U_b##, ##\sqrt{g^2 \left( X^2 - T^2 \right) - v^2}##, is in fact constant along each integral curve of ##U_b##. So we do in fact have ##dY / d\tau## constant on each worldline. But we do
not have ##d Y / d\tau = \gamma v## along each worldline; that is only true on the bottom of the block, where the denominator of each term in ##U_b## becomes ##\sqrt{1 - v^2}##, so the last term does become ##\gamma v##. But at the top of the block, the denominator is larger, so we have ##dY / d\tau < \gamma v##.
What does this mean? It is just a consequence of the fact that, at the top of the block, time "flows" faster than at the bottom. What does this mean for the original constraint we imposed? What is now held constant? The answer is that, in the MCIF of the floor of the rocket, the top of the block should have the
same ordinary velocity ##v## in the ##Y'## direction as the bottom does. But since the top of the rocket/block has faster "time flow" than the bottom, that means that ##dY / d\tau## at the top must be less than ##dY / d\tau## at the bottom, which was equal to ##\gamma v##. And that is what we see in ##U_b##. And, furthermore, we do
not see this in pervect's 4-velocity field, where we have ##U^Y = \gamma v## at the top of the rocket as well as at the bottom--with this 4-velocity field, the top of the block will actually be moving
faster, in the MCIF of the bottom of the rocket, than the bottom is! (That was the other thing that was nagging at me all through this thread.)
Sorry for the long post to add to all the other long posts in this thread.

But I wanted to get all this out while it was fresh in my mind.