If V₁ is the jet velocity and V₀ is the vehicle velocity, then the propulsive efficiency of a rocket is given by Options: A . &nbsp[2(V₀/V₁)]/ [1 + (V₀/V₁)²] B . &nbsp(V₀/V₁)/ [1 + (V₀/V₁)²] C . &nbspV₀/(V₀ + V₁) D . &nbspV₁/(V₀ + V₁)

If V₁ is the jet velocity and V₀ is the vehicle velocity, then the propulsiv

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