A Saturn V rocket with an initial mass m0 of 3 106 kg has a payload that accounts for 27% of this mass,a burn rate of 15 103 kg/s,and a thrust Fth of 35 106 N.The exhaust speed is
A) 1.46 km/s
B) 1.85 km/s
C) 2.09 km/s
D) 2.33 km/s
E) 2.54 km/s
Correct Answer:
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