Answer:
a = 39.2 m/s²
Explanation:
The takeoff acceleration of a missile or a rocket can be expressed by the equation
Where V₀ is the exhaust velocity, m is the mass of the missile, Δm is the mass of gas expelled during a timelapse Δt, and g is gravitational acceleration.
All required data is given by the problem, so now we solve for a:
a = 2.50x10³m/s ÷ 10,000kg * 196kg ÷ 1s - 9.8m/s²
a = 39.2 m/s²