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Rocket Propulsion MCQ
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The O/F ratio in rocket propulsion refers to:
The O/F ratio in rocket propulsion refers to:
A. Oxidizer to fuel mass ratio
B. Output force
C. Overload factor
D. Oxygen flow rate
Explanation:
O/F ratio is the mass ratio of oxidizer to fuel.
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Rocket Propulsion MCQ
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Aerospace Engineering
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