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Two satellites A and B go around a plane...

Two satellites A and B go around a planet in circular orbits of radii 4 R and R respectively. If the speed of the satellite A is 3 V, then the speed of the satellite B will be

A

12 v

B

6 v

C

`(4v)/3`

D

`(3v)/2 `

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The correct Answer is:
To solve the problem of finding the speed of satellite B given the speed of satellite A, we can follow these steps: ### Step-by-Step Solution: 1. **Understand the relationship between gravitational force and centripetal force**: The gravitational force acting on a satellite provides the necessary centripetal force for it to maintain its circular orbit. The gravitational force \( F_g \) is given by: \[ F_g = \frac{GMm}{r^2} \] where \( G \) is the gravitational constant, \( M \) is the mass of the planet, \( m \) is the mass of the satellite, and \( r \) is the radius of the orbit. 2. **Set up the equation for centripetal acceleration**: The centripetal force required for circular motion is given by: \[ F_c = \frac{mv^2}{r} \] where \( v \) is the orbital speed of the satellite. 3. **Equate gravitational force and centripetal force**: Since the gravitational force provides the centripetal force, we can set them equal: \[ \frac{GMm}{r^2} = \frac{mv^2}{r} \] 4. **Cancel the mass of the satellite \( m \)**: Since \( m \) appears on both sides of the equation, we can cancel it out: \[ \frac{GM}{r^2} = \frac{v^2}{r} \] 5. **Rearrange to find the orbital speed**: Multiplying both sides by \( r \) gives: \[ v^2 = \frac{GM}{r} \] Taking the square root, we find: \[ v = \sqrt{\frac{GM}{r}} \] 6. **Relate the speeds of the two satellites**: Since both satellites A and B orbit the same planet, the gravitational constant \( G \) and the mass \( M \) are the same for both. Therefore, the orbital speeds are related to the square root of the inverse of their respective radii: \[ \frac{v_B}{v_A} = \sqrt{\frac{r_A}{r_B}} \] 7. **Substitute the given values**: For satellite A, the radius \( r_A = 4R \) and for satellite B, the radius \( r_B = R \). The speed of satellite A is given as \( v_A = 3V \): \[ \frac{v_B}{3V} = \sqrt{\frac{4R}{R}} = \sqrt{4} = 2 \] 8. **Calculate the speed of satellite B**: Rearranging gives: \[ v_B = 2 \times 3V = 6V \] ### Final Answer: The speed of satellite B is \( 6V \).
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