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. | \(\sqrt{\dfrac{1}{18}} v_e\) | 2. | \(\sqrt{\dfrac{1}{2}} v_e\) |
3. | \(\sqrt{\dfrac{1}{9}} v_e\) | 4. | \(\sqrt{\dfrac{1}{10}} v_e\) |
1. | ![]() |
2. | ![]() |
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4. | ![]() |
A satellite of mass \(M\) is revolving around the Earth in a stationary orbit with a time period \(T.\) If \(10\%\) of the satellite's mass is detached, what will happen to its time period?
1. remain the same
2. increase by \(10\%\)
3. decrease by \(10\%\)
4. decrease by \(20\%\)
1. | \(72\) N | 2. | \(32\) N |
3. | \(28\) N | 4. | \(16\) N |
1. | \(\left(\dfrac{{GM}}{2 {R}}\right)^{\frac{1}{2}} \) | 2. | \(\left(\dfrac{{g} R}{4}\right)^{\frac{1}{2}} \) |
3. | \( \left(\dfrac{2 g}{R}\right)^{\frac{1}{2}} \) | 4. | \(\left(\dfrac{G M}{R}\right)^{\frac{1}{2}}\) |