The planet Mars has two moons, Phobos and Delmos. Phobos has a period of \(7\) hours, \(39\) minutes and an orbital radius of 9.4×103 km. The mass of mars is:
1. 6.48×1023 kg
2. 6.48×1025 kg
3. 6.48×1020 kg
4. 6.48×1021 kg

Subtopic:  Satellite |
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You are given the following data: \(g = 9.81~ \text{m/s}^{2}\), \(R_{E}   =   6 . 37 \times 10^{6}~\text m\), the distance to the moon, \(R = 3 . 84 \times 10^{8}~\text m\) and the time period of the moon’s revolution is 27.3 days. Mass of the Earth \(M_{E}\) in two different ways is:

1.   \(5 . 97 \times 10^{24}  ~ \text{kg and }6 . 02 \times 10^{24}   \text{ kg}\)

2.   \(5 . 97 \times 10^{24}  \text{ kg and }  6 . 02 \times 10^{23}  \text{ kg}\)

3.   \(5 . 97 \times 10^{23}  ~ \text{kg and }6 . 02 \times 10^{24}   \text{ kg}\)

4.   \(5 . 97 \times 10^{23}  \text{ kg and }  6 . 02 \times 10^{23}  \text{ kg}\)

Subtopic:  Satellite |
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Constant \(k   =   10^{- 13} ~ \text s^{2}~ \text m^{- 3}\) in days and kilometres is?

1.   \(10^{- 13} ~ \text d^{2} ~\text{km}^{- 3}\)

2.   \(1 . 33 \times 10^{14}   \text{ dkm}^{- 3}\)

3.   \(10^{- 13} ~ \text d^{2} ~\text {km}\)

4.   \(1 . 33 \times 10^{- 14} \text{  d}^{2} \text{ km}^{- 3}\)

Subtopic:  Satellite |
 57%
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The moon is at a distance of \(3.84\times10^5~\text{km}\) from the earth. Its time period of revolution in days is:
\((\text{Given }k=\dfrac{4\pi^2}{GM_E}=1.33\times10^{-14}~\text{days}^{2}-\text{km}^{-3})\)
1. \(17.3\) days
2. \(33.7\) days
3. \(27.3\) days
4. \(4\) days
Subtopic:  Satellite |
 63%
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A \(400\) kg satellite is in a circular orbit of radius \(2R_E\) (where \(R_E\) is the radius of the earth) about the Earth. How much energy is required to transfer it to a circular orbit of radius \(4R_E\)\(?\)
(Given \(R_E=6.4\times10^{6}\) m)
1. \(3.13\times10^{9}\) J
2. \(3.13\times10^{10}\) J
3. \(4.13\times10^{9}\) J
4. \(4.13\times10^{8}\) J

Subtopic:  Satellite |
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A 400 kg satellite is in a circular orbit of radius 2RE about the Earth. What are the changes in the kinetic and potential energies respectively to transfer it to a circular orbit of radius 4RE. (where RE is the radius of the earth)

1. 3.13×109 J and 6.25×109 J

2. 3.13×109 J and -6.25×109 J

3. -3.13×109 J and -6.25×109 J

4. -3.13×108 J and -6.25×108 J

Subtopic:  Satellite |
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