The objective is to find out the time at which the rocket reaches a speed of 1000m/s (3600km/hr). Analysis We know the following: * Initial mass of the rocket and fuel, 160000kg, or 160 metric tons. * Fuel combustion exhaust velocity relative

Basic Monte Carlo Simulation with normal distribution To use this file: Step 1) consider 2500 the mean of the first term. 100 is the Standard deviation Step 2) consider 2200 the mean of the first term. 200 is the Standard deviatio