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

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

1.	The propulsive power of the rocket is (where v1 = Jet velocity, and v2 = Air-craft velocity)
A.	[A].
B.	[B].
C.	[C].
D.	[D].
Answer» B. [B].

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

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