Question: Extend Prob. 3.104 to the case where the rocket has a linear air drag force F =cV, where c is a constant. Assuming no burnout,

Extend Prob. 3.104 to the case where the rocket has a linear air drag force F =cV, where c 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 c = 0.075 N•s/m to find the angular velocity after 12 s of burning.

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