Iirc, Soyuz also hot stages. So no dramatic zero-g cutoffs between stages.
The third stage also starts before the second stage is completely depleted; this is why there's an "open grate" visible in photos of the rocket (about half way down the stack, see [1]), gives the exhaust somewhere to go before the previous stage is jettisoned. Hot staging is advantageous as you don't need extra ullage motors to deal with propellant being in the wrong place inside the tanks in microgravity. The Soyuz (and other R-7 variants) are brilliantly engineered; There's a reason they're still flying nearly 70 years on.
[1] https://upload.wikimedia.org/wikipedia/commons/thumb/9/9a/So...