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Aerospace Engineering
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Orbital Mechanics MCQ
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The Tsiolkovsky rocket equation relates:
The Tsiolkovsky rocket equation relates:
A. Delta-v, exhaust velocity, and mass ratio
B. Altitude only
C. Orbit period only
D. Fuel consumption only
Explanation:
Tsiolkovsky equation computes delta-v from exhaust velocity and mass ratio.
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Orbital Mechanics MCQ
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Aerospace Engineering
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Kepler’s first law states that the orbit of a planet is:
The orbital period depends primarily on:
A geostationary orbit is characterized by:
Orbital velocity decreases with:
The velocity at perigee is:
Delta-v is used to describe:
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