Answer:
v = 719.2 m / s and   a = 83.33 m / s²
Explanation:
This is a rocket propulsion system where the system is made up of the rocket plus the ejected mass, where the final velocity is
      v - v₀ = [tex]v_{e}[/tex] ln (M₀ / M)
where vâ‚€ is the initial velocity, v_{e} the velocity of the gases with respect to the rocket and Mâ‚€ and M the initial and final masses of the rocket
In this case, if fuel burns at 75 kg / s, we can calculate the fuel burned for the 10 s
      m_fuel = 75 10
      m_fuel = 750 kg
As the rocket initially had a mass of 3000 kg including 1000 kg of fuel, there are still 250 kg, so the mass of the rocket minus the fuel burned is
       M = 3000 -750 = 2250 kg
let's calculate
      v - 0 = 2500 ln (3000/2250)
      v = 719.2 m / s
To calculate the acceleration, let's use the concept of the rocket thrust, which is the force of the gases on it. In the case of the rocket, it is
       Push = v_{e} dM / dt
let's calculate
       Push = 2500  75
       Push = 187500 N
      If we use Newton's second law
       F = m a
       a = F / m
let's calculate
       a = 187500/2250
       a = 83.33 m / s²