Put all answers in a MATLAB script

Problem 2: A model rocket (with mass m = 10 kg) initially at rest on the ground (Zo 0) is launched upward. The motion of the rocket is described by the following differential equations Th dt dt where t is time, z is altitude, w is velocity, and Th is the upward thrust due to the propulsion of the rocket and g is gravity. In this exercise, the upward thrust Th varies with time as follows Th(t) Th(t) Th(t) 675N for 0