| 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. | \(1~\text{year}\) | 2. | \(\sqrt2~\text{year}\) |
| 3. | \(2~\text{year}\) | 4. | \(2\sqrt2~\text{year}\) |
| (A) | a straight line |
| (B) | an ellipse |
| (C) | a parabola |
| (D) | a hyperbola |
| 1. | (A) and (B) only |
| 2. | (A) , (B) and (C) only |
| 3. | (A) , (B) and (D) only |
| 4. | (A) , (B) , (C) and (D) |



