determine the following… (i) Specific impulse (ii) Mass flow rate (iii) Throat diameter (iv) Exit diameter

A rocket is to be designed to produce 5 MN thrust at sea level. The pressure in the combustion chamber is 7 MPa and the temperature is 2800K. If the working fluid is assumed to be a perfect gas with the properties of air at room temperature, determine the following…

(i) Specific impulse

(ii) Mass flow rate

(iii) Throat diameter

(iv) Exit diameter

Engineering

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determine the following… (i) Specific impulse (ii) Mass flow rate (iii) Throat diameter (iv) Exit diameter

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