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The radius of a planet is R1 and a sate...

The radius of a planet is `R_1 ` and a satellite revolves round it in a circle of radius `R_2`. The time period of revolution is T. find the acceleration due to the gravitation of the plane at its surface.

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To find the acceleration due to gravity on the surface of a planet given the radius of the planet \( R_1 \), the radius of the satellite's orbit \( R_2 \), and the time period of the satellite's revolution \( T \), we can follow these steps: ### Step-by-Step Solution: 1. **Understand the relationship between time period, radius, and mass**: The time period \( T \) of a satellite revolving around a planet is given by the formula: \[ T^2 = \frac{4\pi^2 R_2^3}{GM} \] where \( G \) is the universal gravitational constant and \( M \) is the mass of the planet. 2. **Rearrange the formula to find \( GM \)**: From the formula above, we can express \( GM \) as: \[ GM = \frac{4\pi^2 R_2^3}{T^2} \] This will be our equation (1). 3. **Use the formula for acceleration due to gravity**: The acceleration due to gravity \( g \) at the surface of the planet is given by: \[ g = \frac{GM}{R_1^2} \] where \( R_1 \) is the radius of the planet. 4. **Substitute \( GM \) from equation (1) into the formula for \( g \)**: Now, substitute the expression for \( GM \) into the equation for \( g \): \[ g = \frac{1}{R_1^2} \cdot \frac{4\pi^2 R_2^3}{T^2} \] 5. **Final expression for acceleration due to gravity**: Thus, the acceleration due to gravity at the surface of the planet can be expressed as: \[ g = \frac{4\pi^2 R_2^3}{T^2 R_1^2} \] ### Final Answer: The acceleration due to gravity on the surface of the planet is: \[ g = \frac{4\pi^2 R_2^3}{T^2 R_1^2} \]

To find the acceleration due to gravity on the surface of a planet given the radius of the planet \( R_1 \), the radius of the satellite's orbit \( R_2 \), and the time period of the satellite's revolution \( T \), we can follow these steps: ### Step-by-Step Solution: 1. **Understand the relationship between time period, radius, and mass**: The time period \( T \) of a satellite revolving around a planet is given by the formula: \[ T^2 = \frac{4\pi^2 R_2^3}{GM} ...
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