A rocket produces a total thrust of 20,000 N. If the mass flow rate of – McqOptions

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1.	A rocket produces a total thrust of 20,000 N. If the mass flow rate of propellants is 16 kg/s, what will be effective exhaust velocity?
A.	1250 m/s
B.	2500 m/s
C.	625 m/s
D.	5000 m/s
Answer» B. 2500 m/s

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