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An astronaut of mass m is working on a s...

An astronaut of mass m is working on a satellite orbiting the earth at a distance h from the earth's surface the radius of the earth is R while its mass is M the gravitational pull `F_(G)` on the astronaut is

A

Zero since astronaut feels weightless

B

`0 lt F_G lt (GMm)/R^2`

C

`(GMm)/((R+h)^2) lt F_G lt (GMm)/R^2`

D

`F_G=(GMm)/((R+h)^2)`

Text Solution

AI Generated Solution

The correct Answer is:
To find the gravitational pull \( F_G \) on the astronaut working on a satellite orbiting the Earth, we can follow these steps: ### Step 1: Understand the scenario The astronaut of mass \( m \) is in a satellite at a distance \( h \) above the Earth's surface. The radius of the Earth is \( R \), and the mass of the Earth is \( M \). ### Step 2: Determine the distance from the center of the Earth The total distance \( r \) from the center of the Earth to the astronaut is given by: \[ r = R + h \] ### Step 3: Use the formula for gravitational force The gravitational force \( F_G \) acting on the astronaut can be calculated using Newton's law of gravitation: \[ F_G = \frac{G \cdot M \cdot m}{r^2} \] where \( G \) is the universal gravitational constant. ### Step 4: Substitute the expression for \( r \) Substituting \( r = R + h \) into the gravitational force equation, we get: \[ F_G = \frac{G \cdot M \cdot m}{(R + h)^2} \] ### Step 5: Conclusion Thus, the gravitational pull \( F_G \) on the astronaut is: \[ F_G = \frac{G \cdot M \cdot m}{(R + h)^2} \] ### Final Answer Among the given options, the correct one is: \[ F_G = \frac{G \cdot M \cdot m}{(R + h)^2} \]

To find the gravitational pull \( F_G \) on the astronaut working on a satellite orbiting the Earth, we can follow these steps: ### Step 1: Understand the scenario The astronaut of mass \( m \) is in a satellite at a distance \( h \) above the Earth's surface. The radius of the Earth is \( R \), and the mass of the Earth is \( M \). ### Step 2: Determine the distance from the center of the Earth The total distance \( r \) from the center of the Earth to the astronaut is given by: \[ ...
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