a case study on rocket propulsion indicating different phase of changing mass and momentum, factors of acceleration and involvement of Newton's 3rd law of motion
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The propulsion of all rockets is explained by the same physical principle: Newton’s third law of motion.
A rocket’s acceleration depends on three major factors: the exhaust velocity, the rate the exhaust is ejected, and the mass of the rocket.
To achieve the high speeds needed to hop continents, obtain orbit, or escape Earth’s gravity altogether, the mass of the rocket other than fuel must be as small as possible.
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