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A rocket motor with chamber pressure and temperature of 2.04 MPa, 2200 K,  operates at sea level where pressure is 0.1 MPa. Find thrust produced and specific  impulse for propellant consumption of 1.0 kg/s. Take cp = 1500 J/kg K, k = 1.3, g =  9.807 and R = 346 J/kg K. Find also thrust when the pressure inside the nozzle is  50% of initial

A rocket motor with chamber pressure and temperature of 2.04 MPa, 2200 K,  operates at sea level where pressure is 0.1 MPa. Find thrust produced and specific  impulse for propellant consumption of 1.0 kg/s. Take cp = 1500 J/kg K, k = 1.3, g =  9.807 and R = 346 J/kg K. Find also thrust when the pressure inside the nozzle is  50% of initial

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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 A rocket motor with chamber pressure and temperature of 2.04 MPa, 2200 K, 
operates at sea level where pressure is 0.1 MPa. Find thrust produced and specific 
impulse for propellant consumption of 1.0 kg/s. Take cp = 1500 J/kg K, k = 1.3, g = 
9.807 and R = 346 J/kg K. Find also thrust when the pressure inside the nozzle is 
50% of initial

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