A rocket flies at 10,080 kmph with an effective exhaust jet velocity of 1400 m/s and...
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A rocket flies at 10,080 kmph with an effective exhaust jet velocity of 1400 m/s and propellant flow rate of 5.0 kg/s. If the heat of reaction of the propellants is 6500 kJ/kg of the propellant mixture determine: a) Propulsion efficiency and propulsion power, b) engine output and thermal efficiency, and c) overall efficiency. A rocket flies at 10,080 kmph with an effective exhaust jet velocity of 1400 m/s and propellant flow rate of 5.0 kg/s. If the heat of reaction of the propellants is 6500 kJ/kg of the propellant mixture determine: a) Propulsion efficiency and propulsion power, b) engine output and thermal efficiency, and c) overall efficiency. A rocket flies at 10,080 kmph with an effective exhaust jet velocity of 1400 m/s and propellant flow rate of 5.0 kg/s. If the heat of reaction of the propellants is 6500 kJ/kg of the propellant mixture determine: a) Propulsion efficiency and propulsion power, b) engine output and thermal efficiency, and c) overall efficiency.
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Related Book For
Thermodynamics An Interactive Approach
ISBN: 978-0130351173
1st edition
Authors: Subrata Bhattacharjee
Posted Date:
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