What are design dynamics that give the rocket engine higher thrust than a air breathing jet engine of similar size in comparison to a turbo jet engine, turbo fan engine, high by pass turbo fan engine, Scram jet or ram jet. Is it impossible to improve any of these engines to match the performance of the rocket in terms of thrust

What are design dynamics that give the rocket engine higher thrust than an air breathing jet engine of similar size in comparison to a turbo jet engine, turbo fan engine, high by pass turbo fan engine, Scram jet or ram jet. Is it impossible to improve any of these engines to match the performance of the rocket in terms of thrust