Problem #1) CAC IM A simple model of a rocket having two engines capable of applying thrust (N₁ and N₂) is shown. Each engine is located at the distance b away from the rocket's centerline. The rocket has mass m and moment of inertia I. Derive the expressions for the rocket's angular acceleration, Ö, and linear accelerations in the x- and y-directions, aG,x about its mass center using the given variables. aG,x and aG,y'

Problem #1) CAC IM A simple model of a rocket having two engines capable of applying thrust (N₁ and N₂) is shown. Each engine is located at the distance b away from the rocket's centerline. The rocket has mass m and moment of inertia I. Derive the expressions for the rocket's angular acceleration, Ö, and linear accelerations in the x- and y-directions, aG,x about its mass center using the given variables. aG,x and aG,y'