Physics, asked by haroon1979, 3 days ago

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 2800 K. If the working fluid is assumed to be a perfect gas with the properties of air at room temperature, determine the following...

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Answered by mayankgrover2017
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engineeringmechanical engineeringmechanical engineering questions and answersproblems 1. a rocket is to be designed to produce 5 mn of thrust at sea level. the pres- sure in the combustion chamber is 7 mpa and the temperature is 2800 k. if the working fluid is assumed to be a perfect gas with the properties of air at room temperature, determine the following: (a) specific impulse, (b) mass flow rate, (c) throat diameter, (d) exit

Question: PROBLEMS 1. A Rocket Is To Be Designed To Produce 5 MN Of Thrust At Sea Level. The Pres- Sure In The Combustion Chamber Is 7 MPa And The Temperature Is 2800 K. If The Working Fluid Is Assumed To Be A Perfect Gas With The Properties Of Air At Room Temperature, Determine The Following: (A) Specific Impulse, (B) Mass Flow Rate, (C) Throat Diameter, (D) Exit

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PROBLEMS

1. A rocket is to be designed to produce 5 MN of thrust at sea level. The pres-

sure in the combustion chamber is 7

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Transcribed image text: PROBLEMS 1. A rocket is to be designed to produce 5 MN of thrust at sea level. The pres- sure in the combustion chamber is 7 MPa and the temperature is 2800 K. If the working fluid is assumed to be a perfect gas with the properties of air at room temperature, determine the following: (a) specific impulse, (b) mass flow rate, (c) throat diameter, (d) exit diameter. For the same nozzle find (e) thrust at 30-KM altitude; (f) thrust at sea level if chamber pressure were increased to 21 MPa; (g) thrust with hydrogen at the same inlet stagnation conditions; and (h) thrust with stagnation tem- perature increased to 3600 K.

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