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Aerospace Engineering
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Rocket Propulsion MCQ
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The specific impulse of a rocket engine is defined as:
The specific impulse of a rocket engine is defined as:
A. Impulse per unit thrust
B. Thrust per unit mass flow rate of propellant
C. Mass of rocket
D. Velocity of satellite
Explanation:
Specific impulse (Isp) = Thrust / (propellant mass flow rate × g0).
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Rocket Propulsion MCQ
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Aerospace Engineering
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