A launch vehicle has 6 engines operating in parallel which are fed from the same propellant tank. Initially, each engine has an equivalent exhaust velocity of 3500 m/s and consumes 400 kilograms of propellant per second. One of the engines malfunctions and consequently operates at 50% thrust and 120% propellant consumption. Calculate the equivalent exhaust velocity in m/s of all engines if treated as a single engine, including the malfunctioning engine in your calculation.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A launch vehicle has 6 engines operating in parallel which are fed from the same propellant tank.
Initially, each engine has an equivalent exhaust velocity of 3500 m/s and consumes 400 kilograms of
propellant per second.
One of the engines malfunctions and consequently operates at 50% thrust and 120% propellant
consumption. Calculate the equivalent exhaust velocity in m/s of all engines if treated as a single
engine, including the malfunctioning engine in your calculation.
Transcribed Image Text:A launch vehicle has 6 engines operating in parallel which are fed from the same propellant tank. Initially, each engine has an equivalent exhaust velocity of 3500 m/s and consumes 400 kilograms of propellant per second. One of the engines malfunctions and consequently operates at 50% thrust and 120% propellant consumption. Calculate the equivalent exhaust velocity in m/s of all engines if treated as a single engine, including the malfunctioning engine in your calculation.
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