1.

A rocket engine moving at 500 m/s produces a total thrust of 9563 N, consuming propellants at the rate of 4.55 kg/s. The energy content of the propellants is 5.35 MJ/kg. Find the effective exhaust velocity.

A. 2100 m/s
B. 3936 m/s
C. 1555 m/s
D. 1400 m/s
Answer» B. 3936 m/s


Discussion

No Comment Found