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MSC,MBA(IT)
Standford
Jun-1997 - Sep-2000
IT Manager
Honeywell
Aug-2001 - Present
In the early stages of the Saturn V rocket's launch, mass was ejected at about 15,000 kg/s, with a speed vex ≈ 2500 m/s relative to the rocket. What was the thrust on the rocket? Convert this to tons (1 ton ti 9000 newton’s) and compare with the rocket's initial weight (about 3000 tons).
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