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. assume g= 10m/s^2

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1) 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.

assume g= 10m/s^2

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