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If a graph is plotted between T^(2) and ...

If a graph is plotted between `T^(2) and r^(3)` for a planet, then its slope will be be (where `M_(S)` is the mass of the sun)

A

A. `(4pi^(2))/(GM_(S))`

B

B.`(GM_(S))/(4pi)`

C

C. `4piGM_(S)`

D

`D. GM_(S)`

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The correct Answer is:
To solve the problem, we need to determine the slope of the graph plotted between \( T^2 \) (the square of the orbital period of a planet) and \( r^3 \) (the cube of the radius of the orbit) for a planet orbiting the Sun. We will use Kepler's Third Law of planetary motion, which states that the square of the period of orbit \( T \) is directly proportional to the cube of the semi-major axis of its orbit \( r \). ### Step-by-Step Solution: 1. **Understanding the Relationship**: According to Kepler's Third Law, we have the relation: \[ T^2 \propto r^3 \] This implies that: \[ T^2 = k \cdot r^3 \] where \( k \) is a constant. 2. **Expressing the Constant \( k \)**: For a planet orbiting the Sun, we can express \( k \) in terms of the gravitational constant \( G \) and the mass of the Sun \( M_S \): \[ k = \frac{4 \pi^2}{G M_S} \] Thus, we can rewrite the equation as: \[ T^2 = \frac{4 \pi^2}{G M_S} \cdot r^3 \] 3. **Identifying the Slope**: From the equation \( T^2 = \frac{4 \pi^2}{G M_S} \cdot r^3 \), we can see that if we plot \( T^2 \) on the y-axis and \( r^3 \) on the x-axis, the slope of the line will be: \[ \text{slope} = \frac{4 \pi^2}{G M_S} \] 4. **Conclusion**: Therefore, the slope of the graph plotted between \( T^2 \) and \( r^3 \) is: \[ \text{slope} = \frac{4 \pi^2}{G M_S} \] This corresponds to option A. ### Final Answer: The slope of the graph between \( T^2 \) and \( r^3 \) is \( \frac{4 \pi^2}{G M_S} \) (Option A). ---

To solve the problem, we need to determine the slope of the graph plotted between \( T^2 \) (the square of the orbital period of a planet) and \( r^3 \) (the cube of the radius of the orbit) for a planet orbiting the Sun. We will use Kepler's Third Law of planetary motion, which states that the square of the period of orbit \( T \) is directly proportional to the cube of the semi-major axis of its orbit \( r \). ### Step-by-Step Solution: 1. **Understanding the Relationship**: According to Kepler's Third Law, we have the relation: \[ T^2 \propto r^3 \] ...
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