At liftoff, the engines of the Saturn V rocket consumed 14,000 kg/s of fuel and exhausted the combustion products at 2900 m/s. What was the total upward force (thrust) provided by the engines?
A) 3.77 * 107 N
B) 7.54* 107 N
C) 1.47 * 108 N
D) 4.06 * 107 N
Correct Answer:
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