What is the thrust developed by the rocket

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Reference no: EM13536292

An aircraft uses a rocket-assisted takeoff unit (RATO) that is capable of discharging 47.0 kg of gas in 10.0 s with an exhaust velocity of 1100 m/s. The 3000 kg aircraft, on an ordinary takeoff without RATO, requires a distance of 400 m to reach a lift-off speed of 250 km/hr with a constant propeller thrust. What is the thrust developed by the rocket?

Reference no: EM13536292

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