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A satellite is orbiting the earth in an ...

A satellite is orbiting the earth in an orbit with a velocity `4 km//s`, then the acceleration due to gravity at that height is (in `ms^(-2)`)

A

`0.4`

B

`0.62`

C

`0.87`

D

`1.21`

Text Solution

AI Generated Solution

The correct Answer is:
To find the acceleration due to gravity at the height where a satellite is orbiting the Earth with a velocity of 4 km/s, we can use the relationship between gravitational force and centripetal acceleration. ### Step-by-step Solution: 1. **Convert the velocity to meters per second**: The velocity of the satellite is given as 4 km/s. \[ v = 4 \text{ km/s} = 4 \times 10^3 \text{ m/s} \] 2. **Use the formula for centripetal acceleration**: The centripetal acceleration \( a_c \) of the satellite can be expressed as: \[ a_c = \frac{v^2}{r} \] where \( r \) is the distance from the center of the Earth to the satellite. 3. **Relate centripetal acceleration to gravitational acceleration**: The gravitational force provides the necessary centripetal force for the satellite's orbit. Thus, we have: \[ a_c = g' = \frac{GM}{r^2} \] where \( g' \) is the acceleration due to gravity at the height of the satellite, \( G \) is the universal gravitational constant, and \( M \) is the mass of the Earth. 4. **Set the equations equal**: Since both expressions represent the acceleration at the height of the satellite, we can set them equal to each other: \[ \frac{v^2}{r} = \frac{GM}{r^2} \] 5. **Rearranging the equation**: Multiply both sides by \( r^2 \): \[ v^2 \cdot r = GM \] Now, we can express \( g' \) in terms of \( v \): \[ g' = \frac{v^2}{r} \] 6. **Substituting the values**: We need to find \( r \). We can rearrange the equation to find \( r \): \[ r = \frac{GM}{v^2} \] However, we can also express \( g' \) in terms of known values. The radius of the Earth \( R \) is approximately \( 6.37 \times 10^6 \) m, and the gravitational acceleration at the surface \( g \) is approximately \( 9.81 \, \text{m/s}^2 \). 7. **Calculate \( g' \)**: Using the formula: \[ g' = \frac{v^2}{R} \] We can substitute \( v = 4 \times 10^3 \text{ m/s} \): \[ g' = \frac{(4 \times 10^3)^2}{6.37 \times 10^6} \] \[ g' = \frac{16 \times 10^6}{6.37 \times 10^6} \approx 2.51 \, \text{m/s}^2 \] 8. **Final Calculation**: After calculating, we find that the acceleration due to gravity at that height is approximately \( 2.51 \, \text{m/s}^2 \). ### Final Answer: The acceleration due to gravity at that height is approximately \( 2.51 \, \text{m/s}^2 \).

To find the acceleration due to gravity at the height where a satellite is orbiting the Earth with a velocity of 4 km/s, we can use the relationship between gravitational force and centripetal acceleration. ### Step-by-step Solution: 1. **Convert the velocity to meters per second**: The velocity of the satellite is given as 4 km/s. \[ v = 4 \text{ km/s} = 4 \times 10^3 \text{ m/s} ...
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