Compute the drag force on a missile 0.6 cm in diameter moving at 250 m/s at low altitude,where the density of air is 1:2 kg=m3. Assume C = 0.8.

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Compute the drag force on a missile 0.6 cm in diameter moving at 250 m/s at low altitude,where the density of air is 1:2 kg=m3. Assume C = 0.8.

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