a rocket is moving with a velocity v1 while the velocity of gases ejecting from the rocket is v2 then velocity of gases plume with respect to rocket is
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since linear momentum is conserved
mass (rocket)×velocity (rocket) = mass (gases)×velocity(gases)
v (g)/v (r)= mass (r)/ mass (g)
mass (rocket)×velocity (rocket) = mass (gases)×velocity(gases)
v (g)/v (r)= mass (r)/ mass (g)
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