Question: A rocket has the following data: Propellant flow rate = 5 kg/s Nozzle exit diameter =10 cm Nozzle exit pressure = 1.02 bar Ambient
A rocket has the following data: Propellant flow rate = 5 kg/s Nozzle exit diameter =10 cm Nozzle exit pressure = 1.02 bar Ambient pressure = 1.013 bar Thrust chamber pressure = 20 bar Thrust = 7 KN Determine the effective jet velocity, actual jet velocity specific impulse and specific propellant consumption.
Step by Step Solution
3.36 Rating (143 Votes )
There are 3 Steps involved in it
The detailed ... View full answer
Get step-by-step solutions from verified subject matter experts
