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 × 10^7 N
c. 1.47 × 10^8 N
b. 7.54 × 10^7 N
d. 4.06 × 10^7 N


D

Physics & Space Science

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Physics & Space Science