Explain how the conservation of momentum is responsible for the propulsion of a rocket.
Rocket propulsion is an example of conservation of momentum
As momentum is given in one direction to exhaust gases, it is given in the other direction to the rocket.
Consider a rocket of finite mass m1 and amount of fuel m2.
in the beginning, the rocket is stationary and no exhaust gases are expelled.
p(net ) = 0
after the mass is ejected
p(net) = p(rocket) + p(fuel)
p(net) = m1v1 + m2v2
since v1 and v2 are in opposite direction, the rocket gets a net momentum which is equal to the momentum of fuel ejected
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