Answer:
(b) 2.40 x
kg/s
Step-by-step explanation:
Given that: Total mass of the rocket = 3.003 x
kg
acceleration of the rocket = 36.0 m

speed of the exhausted gases = 4.503 x
m/s
Rate at which rocket was initially burning fuel =

But,
time =

=

= 125.0833 s
So that;
Rate at which rocket was initially burning fuel =

= 2400.8001
= 2.40 x
kg/s
Therefore, the initial rate at which the rocket burn fuel is 2.40 x
kg/s.