Let be the gas mass ejected in a short interval, and let be the stationary dust mass acquired. The rocket mass change is . Before the interval the momentum of the rocket and this dust is , because the incoming dust is at rest. Afterwards it is
to first order; changing the gas ejection speed by affects only second-order terms. Momentum conservation, with no external force, therefore gives
Dividing by the time interval produces the rocket equation with stationary mass accretion:
The incoming material's zero initial momentum is essential: accelerating it to the rocket's speed consumes part of the thrust.

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