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Establish the following relations for a rocket v =Vo +Be In Mo/M |
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Answer» The thrust DEVELOPED by a rocket-motor is given by F=mv+A(P 1 −P 2 ) where m is the mass of the gas EJECTED per unit time, v is velocity of the gas, A is area of cross-section of the NOZZLE, P 1 and P 2 are the pressures of the exhaust gas and surrounding ATMOSPHERE. The formula is dimensionally |
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