A
Reentry Breakup Recorder is used to record data while an unmanned spacecraft breaks up when returning from a Low Earth Orbit re-entering the atmosphere.
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Comparison of Reentry Breakup Measurements for Three Atmospheric Reentries (PDF) has been presented in A.D. 2013.
The three vehicles are cylindrical, about 10m long and 4.5m diameter, weight more than 10 metric tons.
On page 11 the authors show altitude in km over time in seconds, as well as acceleration in g (=9.81m/s^2).

All three altitude-curves for the three vehicles start with a nearly linear section from 120km down to 70km. Accordingly the vehicles have a constant vertical velocity and zero vertical acceleration. The diagram shows that for the first 100 seconds the acceleration vector is zero.
But that is impossible. Air friction deceleration cannot on the one hand cancel gravity in the vertical direction and at the same time be zero in the horizontal direction. The air friction deceleration vector points against the flight path direction. The flight path angle stays constant at -1.663° (for ATV-3/REBR4), see page 10. The graph obviously has little to do with reality.
Also, mass density ρ of air is proportional to e
-h/8400m. We have e
-70000m/8400m / e
-120000m/8400m = e
50/8.4 = 384. Mass density ρ of air at 70km is 384 times higher than at 120km. Gravity on the other hand increases by 2% from 120km down to 70km. How can a 384 times thicker air cause virtually the same amount of friction, while velocity doesn't change? That's ridiculous!
Something is rotten in space flight.
P.S.: A more detailed version of the above linked docuмent can be found
here.