The acceleration of the rocket will be "56.2 m/s²".
According to the question,
The initial speed during launch,
The speed at fuel running out point,
Height,
      = 1250 m
As we know,
→ [tex]vf^2 = u^2+2ah[/tex]
or,
→   [tex]a = \frac{v_f^2-u^2}{2h}[/tex]
By putting the values, we get
→    [tex]=\frac{(375)^2-(0)^2}{2\times 1250}[/tex]
→    [tex]=\frac{140625}{2500}[/tex]
→    [tex]= 56.2 \ m/s^2[/tex]
Thus the above solution is correct.
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