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Question 7
Derive an expression to show that for satellites in a circular orbit $r^2 \propto T^2$ where $T$ is the period of orbit and $r$ is the radius of the orbit.
Step 1
Answer
The centripetal force acting on a satellite in a circular orbit is given by:
where is the mass of the satellite, is its orbital speed, and is the radius of the orbit. This force must equal the gravitational force acting on the satellite:
where is the gravitational constant, and is the mass of the planet around which the satellite orbits.
Step 2
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