M is the rocket’s mass at any given moment t.
The rocket’s velocity is v.
The mass of the gas expelled during the time interval t is m.
As a result, K = 1/2 u2∆m
M is the rocket’s mass at any given moment t.
The rocket’s velocity is v.
The mass of the gas expelled during the time interval t is m.
As a result, K = 1/2 u2∆m