The thrust developed derives from
F = Ve(w)/g where F = thrust, w = the propelant flow rate and g = the acceleration due to gravity.
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.
2 answers
it is just F= V(flow rate)
U don't divide by the gravity
U don't divide by the gravity