What is the final altitude of the rocket when all the fuel


How high will your model rocket fly? Assume the model rocket weighs 5 kg and the fuel weighs 0.5 kg. Assume a mass flow rate of 0.1 kg/s and an exhaust velocity of 15 m/s. What is the final altitude of the rocket when all the fuel is consumed? How good was the constant-gravity assumption?

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Mechanical Engineering: What is the final altitude of the rocket when all the fuel
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