Asked by kalli sarik

calculate the force exerted on a rocket given that the propelling gases are expelled at a rate of 1000 kg/s with a speed of 60,000 m/s.
Answered by tchrwill
The thrust developed derives from

F = Ve(w)/g where F = thrust, w = the propelant flow rate and g = the acceleration due to gravity.
Answered by Diego1
it is just F= V(flow rate)

U don't divide by the gravity
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