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A rocket engine has the following data: Effective jet velocity = 1400 m/s Flight to jet speed ratio = 0.82 Oxidizer flow rate =
A rocket engine has the following data: Effective jet velocity = 1400 m/s Flight to jet speed ratio = 0.82 Oxidizer flow rate = 3.5 kg/s Fuel flow rate = 1.2 kg/s Heat of reaction per kg of the exhaust gas = 2600 KJ/kg. Calculate the thrust, specific impulse, propulsive efficiency, thermal efficiency and overall efficiency.
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Cornerstones of Financial Accounting
Authors: Jay Rich, Jeff Jones
4th edition
978-1337690881, 9781337669450, 1337690880, 1337690899, 1337669458, 978-1337690898
