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An airplane weighing 24000 N and with a wing reference area of ​​20 m² climbs at...

An airplane weighing 24000 N and with a wing reference area of ​​20 m² climbs at an actual air speed of 120 m / s. Since the impulse received from the engine is 10000 N, the drag coefficient of the plane is 0.05 and the air density at the current altitude is 1 kg / m³, what is the vertical climbing speed of the plane?

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