If R is the radius of the orbit of a planet and T is the time period of the planet, then which of the following graphs correctly shows the motion of a planet revolving around the sun?

1.     2.
3. 4.  

Subtopic:  Kepler's Laws |
 78%
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The figure shows a planet in an elliptical orbit around the sun (S). The ratio of the momentum of the planet at point A to that at point B is:

                              

1. r1r2 2.  r12r22
3. r2r1 4.  r22r12
Subtopic:  Kepler's Laws |
 59%
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Three identical point masses, each of mass 1 kg lie at three points (0, 0), (0, 0.2 m), (0.2 m, 0). The net gravitational force on the mass at the origin is:
1. \(6.67\times 10^{-9}(\hat i +\hat j)~\text{N}\)
2. \(1.67\times 10^{-9}(\hat i +\hat j) ~\text{N}\)
3. \(1.67\times 10^{-9}(\hat i -\hat j) ~\text{N}\)
4. \(1.67\times 10^{-9}(-\hat i -\hat j) ~\text{N}\)

Subtopic:  Newton's Law of Gravitation |
 66%
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Two particles of mass \(\mathrm{m}\) and \(\mathrm{4m}\) are separated by a distance \(\mathrm{r}.\) Their neutral point is at:

1.  r2 from m

2.  r3 from 4m

3.  r3 from m

4.  r4 from 4m

Subtopic:  Newton's Law of Gravitation |
 74%
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A body of mass m is situated at a distance 4Re above the Earth's surface, where Re is the radius of the Earth. What minimum energy should be given to the body so that it may escape? 

1. mgRe 2. 2mgRe
3. mgRe/5 4. mgRe/16
Subtopic:  Gravitational Potential Energy |
 74%
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A satellite of mass m revolving around the earth in a circular orbit of radius r has its angular momentum equal to L about the centre of the earth. The potential energy of the satellite is: 

1.  -L22mr 2. -2L2mr2
3. -3L2m2r2 4. -L2mr2
Subtopic:  Satellite |
 54%
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The value of acceleration due to gravity at a height of 800 km from the surface of the earth (radius of the earth is 6400 km and value of acceleration due to gravity on the earth's surface is 981 cm/s2) is:

1. \(775 \mathrm{~cm} / \mathrm{s}^2 \) 2. \(872 \mathrm{~cm} / \mathrm{s}^2 \)
3. \(981 \mathrm{~cm} / \mathrm{s}^2 \) 4. \(Zero\)

Subtopic:  Acceleration due to Gravity |
 71%
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Two satellites S1 and S2 are revolving around a planet in coplanar and concentric circular orbits of radii Rand R2 in the same direction respectively. Their respective periods of revolution are 1 hr and 8 hr. The radius of the orbit of satellite S1 is equal to 104 km. Find the relative speed when they are closest to each other. 

1. 2π×104 kmph

2. π×104 kmph

3. π2×104 kmph

4. π3×104 kmph 

Subtopic:  Kepler's Laws |
 56%
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The gravitational potential energy of an isolated system of three particles, each of mass \(\mathrm{m}\) placed at three corners of an equilateral triangle of side \(\mathrm{l}\) is: 

1. \(-Gm \over \mathrm{l}^2\) 2. \(-Gm^2 \over 2\mathrm{l}\)
3. \(-2Gm^2 \over \mathrm{l}\) 4. \(-3Gm^2 \over \mathrm{l}\)
Subtopic:  Gravitational Potential Energy |
 87%
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A planet is revolving around a massive star in a circular orbit of radius R. If the gravitational force of attraction between the planet and the star is inversely proportional to R3, then the time period of revolution T is proportional to:

1. R5

2. R3

3. R2

4. R

Subtopic:  Satellite |
 63%
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