Extend Prob. 3.104 to the case where the rocket has a quadratic air drag force F =kV2, where k is a constant. Assuming no burnout, solve for ω(t) and find the terminal angular velocity, i.e., the final motion when the angular acceleration is zero. Apply to the case Mo = 6 kg, R = 3 m, m = 0.05 kg/s, Ve = 1100 m/s, and k = 0.0011 N•s2/m2 to find the angular velocity after 12 s of burning.