the4thcafeavenue
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can anyone explain the concept of rocket propulsion, in other words, M*delta(V)=delta(m)*Ve?
Thanks guyz
Thanks guyz
Rocket propulsion operates on the principle defined by the rocket equation, M*delta(V)=delta(m)*Ve, which illustrates the relationship between a rocket's mass, its change in velocity, the mass expelled, and the exhaust velocity. The process involves expelling exhaust gases at high speed in one direction, resulting in thrust that propels the rocket in the opposite direction, adhering to Newton's third law of motion. To achieve increased speed, a rocket must either reduce its mass or enhance the exhaust velocity, necessitating the use of substantial fuel reserves.
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