The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity) Options: A . &nbsp(v₁² -v₂²)/2g B . &nbsp(v₁ - v₂)²/2g C . &nbsp(v₁² -v₂²)/g D . &nbsp(v₁ - v₂)²/g

The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Air

Question

The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

Options:

A . (v₁² -v₂²)/2g

B . (v₁ - v₂)²/2g

C . (v₁² -v₂²)/g

D . (v₁ - v₂)²/g

Answer: Option A

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