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Question

The propulsive power of the rocket is (where v1 = Jet velocity, and v2 = Air-craft velocity)
Options:
A .  `(V_1^2 - V_2^2)/(2g)`
B .  `((V_1 - V_2)^2)/(2g)`
C .  `(V_1^2 - V_2^2)/(g)`
D .  `((V_1 - V_2)^2)/(g)`
Answer: Option A



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