1. | \(mr\) | 2. | \(\dfrac{m}{r}\) |
3. | \(m\sqrt r\) | 4. | \(\dfrac{m}{\sqrt r}\) |
Assertion (A): | The ratio \(R^3/T^2,\) where \(R\) is the radius of the orbit and \(T\) is the time period in the orbit of a satellite of the earth, depends only on the mass of the earth, and not on that of the satellite. |
Reason (R): | This can be easily concluded by the application of Newton's law of gravitation together with Newton's laws of motion to the motion of the satellite in orbit. |
1. | Both (A) and (R) are True and (R) is the correct explanation of (A). |
2. | Both (A) and (R) are True but (R) is not the correct explanation of (A). |
3. | (A) is True but (R) is False. |
4. | (A) is False but (R) is True. |
\(r\) | distance from sun \(S\) |
\(v\) | speed in orbit |
\(K\) | kinetic energy |
\(U\) | potential energy |
Statement I: | The kinetic energy of a planet is maximum when it is closest to the sun. |
Statement II: | The time taken by a planet to move from the closest position (perihelion) to the farthest position (aphelion) is larger for a planet that is farther from the sun. |
1. | Statement I is incorrect and Statement II is correct. |
2. | Both Statement I and Statement II are correct. |
3. | Both Statement I and Statement II are incorrect. |
4. | Statement I is correct and Statement II is incorrect. |
1. | A or B |
2. | A or B or C |
3. | A or B or D |
4. | A or B or C or D |
1. | \(\dfrac{4}{\pi^2}\) | 2. | \(\dfrac{1}{4\pi^2}\) |
3. | \(\dfrac{2}{\pi^2}\) | 4. | \(\dfrac{1}{2\pi^2}\) |