Arocket burns fuel at a rate of 180 kg/s and exhausts the gas at a relative speed of 1 km/s. find the thrust of the rocket. answer in units of mn.

0.18 MN

Explanation:

m = Mass

t = Time taken

u = Initial velocity = 0

v = Final velocity = 1 km/s

= Mass flow rate = 180 kg/s

Force is given by

The thrust on the rocket is 0.18 MN

explanation:

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