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Home
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Aerospace Engineering
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Rocket Propulsion MCQ
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The thrust produced by a rocket is given by:
The thrust produced by a rocket is given by:
A. Mass flow × exhaust velocity + pressure difference term
B. Lift × drag
C. Weight × velocity
D. Fuel mass × altitude
Explanation:
Thrust = ṁ × ve + (pe – pa)Ae.
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Rocket Propulsion MCQ
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Aerospace Engineering
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