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On the press conference they mentioned the RCS was used to orient the craft with the most sturdy part facing down for the ocean impact.

Otherwise I would also just bet on RCS venting like in Apollo.

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There should be an opposite thruster for each axis. I wonder if the short bursts were due to heating limits.
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There are opposed thrusters, but I assume that in atmosphere and under parachute canopy it’s harder to make sure they are perfectly opposed.

Heating likely plays a role as well.

I am not a rocket engineer, but I have read How Apollo Flew to the Moon and Ignition!: an informal history of liquid rocket propellants, both of which cover these issues. Highly recommended.

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The short bursts are just the period of the control cycles. Control cycle starts, loop sees error, commands thrust; next control cycle starts, loop sees error is nulled (or in deadband), commands no thrust.
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