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The height of communication statellite f...

The height of communication statellite from the surface of the earth is approximately

A

`36 xx 10^(3) km`

B

`36 km`

C

`36 xx 10^(4) km`

D

`36 xx 10^(2) km`

Text Solution

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The correct Answer is:
To determine the height of a communication satellite from the surface of the Earth, we can follow these steps: ### Step-by-Step Solution: 1. **Understanding Geostationary Satellites**: - Geostationary satellites are used for communication purposes. They orbit the Earth at a height where they can remain stationary relative to a point on the Earth's surface. 2. **Height Calculation**: - The height \( h \) of a geostationary satellite can be derived from the formula: \[ h = \frac{T^2 \cdot g \cdot R^2}{4 \pi^2} - R \] where: - \( T \) is the time period of the satellite (24 hours), - \( g \) is the acceleration due to gravity (approximately \( 9.8 \, \text{m/s}^2 \)), - \( R \) is the radius of the Earth (approximately \( 6.4 \times 10^6 \, \text{m} \)). 3. **Convert Time Period to Seconds**: - Since \( T \) is given in hours, convert it to seconds: \[ T = 24 \, \text{hours} = 24 \times 60 \times 60 = 86400 \, \text{seconds} \] 4. **Substituting Values**: - Substitute \( T \), \( g \), and \( R \) into the formula: \[ h = \frac{(86400)^2 \cdot 9.8 \cdot (6.4 \times 10^6)^2}{4 \pi^2} - 6.4 \times 10^6 \] 5. **Calculating the Height**: - After performing the calculations, we find: \[ h \approx 3.6 \times 10^7 \, \text{meters} \] 6. **Convert to Kilometers**: - To convert meters to kilometers, divide by 1000: \[ h \approx 3.6 \times 10^7 \, \text{m} = 36 \times 10^3 \, \text{km} \] 7. **Final Answer**: - The height of the communication satellite from the surface of the Earth is approximately \( 36 \times 10^3 \, \text{km} \). ### Final Answer: The height of the communication satellite from the surface of the Earth is approximately \( 36 \times 10^3 \, \text{km} \). ---
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The orbital velocity of a satellite is given by the expression V = sqrt((GM)/(R + h)) , here M is the mass of the Earth, R is the radius of the Earth and 'h' is the height of the satellite from the surface of the Earth. Explain the reasons why the geostationary satellite is not possible to set in orbit around the Earth at two different heights from the surface of the Earth.

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Knowledge Check

  • When the height of a satellite increases from the surface of the earth.

    A
    `PE` decreases,`KE` increases
    B
    `PE` decreases,`KE` decreases
    C
    `PE` increases,`KE` decreases
    D
    `PE` increases,`KE` increases
  • What is the approximate height of a geostationary satellite from the surface of the earth?

    A
    981 km
    B
    15000 km
    C
    35,000 km
    D
    55,000 km
  • If height of a satellite from the surface of earth is increased , then its

    A
    Potential energy will increase
    B
    Kinetic energy will decrease
    C
    Total energy will increase
    D
    All of these
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