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 (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, ...

If linear resistive drag is added to Prob 3104 the ...

Extend Prob. 3.104 to the case where the rocket has a linear air drag force F =cV,

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, 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.