\(r\) | distance from sun \(S\) |
\(v\) | speed in orbit |
\(K\) | kinetic energy |
\(U\) | potential energy |
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1. | \(2\) km/s | 2. | \(2\sqrt2\) km/s |
3. | \(2(\sqrt2-1)\) km/s | 4. | \(2(\sqrt2+1)\) km/s |
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1. | \(4\) | 2. | \(2\) |
3. | \(\dfrac12\) | 4. | \(\dfrac14\) |
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Statement I: | The gravitational force exerted by the Sun on the Earth is reduced when the Moon is between the Earth and the Sun. |
Statement II: | The gravitational force exerted by the Sun on the Earth is reduced when the Moon is opposite to the Sun, relative to the Earth. |
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. |
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Statement I: | The gravitational force acting on a particle depends on the electric charge of the particle. |
Statement II: | The gravitational force on an extended body can be calculated by assuming the body to be a particle 'concentrated' at its centre of mass and applying Newton's law of gravitation. |
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. |
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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. |
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1. | \(3F\) | 2. | \(2F\) |
3. | \(4F\) | 4. | \(F\) |
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1. | \(\dfrac{GMm}{r^2}+\dfrac{2Gm^2}{r^2}\) |
2. | \(\dfrac{GMm}{r^2}+\dfrac{\sqrt3Gm^2}{r^2}\) |
3. | \(\dfrac{GMm}{r^2}+\dfrac{Gm^2}{\sqrt3r^2}\) |
4. | \(\dfrac{GMm}{r^2}+\dfrac{2Gm^2}{\sqrt3r^2}\) |
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1. | \(mr\) | 2. | \(\dfrac{m}{r}\) |
3. | \(m\sqrt r\) | 4. | \(\dfrac{m}{\sqrt r}\) |
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1. | \(U > mgh\) |
2. | \(U < mgh\) |
3. | \(U = mgh\) |
4. | \(h,\) considered relative to the radius of the earth. | any of the above may be true depending on the value of
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