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During launcher ascent, dynamic pressure evolution is describe in
this answer for the Saturn V.
I suppose this is comparable from one launcher to another.

Given the protections designed for reentry, I suppose dynamic pressure involved during reentry are more important than during ascent.

What does this evolution looks like for reentry?
Do it looks like the same (bell shape increase and decrease with almost the same shape)? If the answer is quite different from one spaceship to another,
this question can be narrowed to Apollo or other manned ships.

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For capsule reentry, the Q profile is a bell-shaped curve, narrower than the ascent profile, slightly gentler in slope at the start and steeper at the end.

Here's what it looks like for a steep 40g ballistic (from Aerothermal Analysis of a Sample-Return Reentry Capsule; the dot-dash line is the dynamic pressure curve):

enter image description here

For a crewed capsule the dynamic pressure peak is not quite as narrow and sharp, but the overall shape would be similar; for a 'skip-entry' trajectory there may be multiple pressure peaks instead of a single one. Here's a plot from flight testing of the Orion capsule (blue simulated, red measured):

enter image description here

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Perhaps surprisingly, at least for an aerospace plane like the Shuttle, entry dynamic pressure is maximum once you go subsonic.

enter image description here

It doesn't get anywhere near the ~600 psf experienced during ascent.

source (p. 239)

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