At liftoff, the engines of the Saturn V rocket consumed 12 500 kg/s of fuel and exhausted the combustion products at 2 700 m/s. What was the total upward force (thrust) provided by the engines?

a. 3.38E+7 N
b. 4.63E+6 N
c. 2.16E+5 N
d. 3.48E+7 N
e. 3.28E+7 N


a

Physics & Space Science

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