Given:
Mass of the rocket, $m = 125 \, \text{kg}$
Thrust force of the engine, $F = 1720 \, \text{N}$
Using Newton's second law, $F = ma$, where $F$ is the net force, $m$ is the mass, and $a$ is the acceleration.
Therefore, $a = \frac{F}{m} = \frac{1720 \,
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