Home
Class 11
PHYSICS
A geostationary satellite orbits the ear...

A geostationary satellite orbits the earth at a height of nearly 36,000 km from the surface of earth. What is the potential due to earth's gravity at the site of this satellite? ( Take the potential energy at infinity to be zero). Mass of the earth `6.0 xx 10^(24) kg`, radius = 6400km.

Text Solution

AI Generated Solution

The correct Answer is:
To find the gravitational potential at the site of a geostationary satellite, we can use the formula for gravitational potential \( V \) at a distance \( r \) from the center of the Earth: \[ V = -\frac{G M}{r} \] where: - \( G \) is the gravitational constant, approximately \( 6.67 \times 10^{-11} \, \text{N m}^2/\text{kg}^2 \) - \( M \) is the mass of the Earth, given as \( 6.0 \times 10^{24} \, \text{kg} \) - \( r \) is the distance from the center of the Earth to the satellite. ### Step 1: Calculate the distance \( r \) The distance \( r \) is the sum of the Earth's radius and the height of the satellite above the Earth's surface. Given: - Radius of the Earth \( R = 6400 \, \text{km} = 6400 \times 10^3 \, \text{m} \) - Height of the satellite \( h = 36000 \, \text{km} = 36000 \times 10^3 \, \text{m} \) Now, calculate \( r \): \[ r = R + h = (6400 \times 10^3) + (36000 \times 10^3) = 6400 \times 10^3 + 36000 \times 10^3 = 42600 \times 10^3 \, \text{m} \] ### Step 2: Substitute values into the potential formula Now we substitute \( G \), \( M \), and \( r \) into the potential formula: \[ V = -\frac{G M}{r} \] Substituting the values: \[ V = -\frac{(6.67 \times 10^{-11}) \times (6.0 \times 10^{24})}{42600 \times 10^3} \] ### Step 3: Calculate the potential \( V \) Now we perform the calculation: \[ V = -\frac{(6.67 \times 10^{-11}) \times (6.0 \times 10^{24})}{42600 \times 10^3} \] Calculating the numerator: \[ 6.67 \times 10^{-11} \times 6.0 \times 10^{24} = 4.002 \times 10^{14} \] Now calculate the denominator: \[ 42600 \times 10^3 = 4.26 \times 10^7 \] Now divide the two results: \[ V = -\frac{4.002 \times 10^{14}}{4.26 \times 10^7} \approx -9.39 \times 10^6 \, \text{J/kg} \] ### Final Answer The potential due to Earth's gravity at the site of the geostationary satellite is approximately: \[ V \approx -9.39 \times 10^6 \, \text{J/kg} \]

To find the gravitational potential at the site of a geostationary satellite, we can use the formula for gravitational potential \( V \) at a distance \( r \) from the center of the Earth: \[ V = -\frac{G M}{r} \] where: - \( G \) is the gravitational constant, approximately \( 6.67 \times 10^{-11} \, \text{N m}^2/\text{kg}^2 \) ...
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    ICSE|Exercise SELECTED PROBLEMS[FROM GRAVITATIONAL POTENTIAL ENERGY]|4 Videos
  • GRAVITATION

    ICSE|Exercise SELECTED PROBLEMS[FROM ESCAPE VELOCITY ]|20 Videos
  • GRAVITATION

    ICSE|Exercise SELECTED PROBLEMS[FROM VARIATION OF G WITH ALTITUDE, LATITUDE, DEPTH]|14 Videos
  • FRICTION

    ICSE|Exercise Selected problems|30 Videos
  • INTERNAL ENERGY

    ICSE|Exercise SELECTED PROBLEMS (FROM HEAT ENGINES)|21 Videos

Similar Questions

Explore conceptually related problems

A geostationary satellite is orbiting the earth at a height of 6R above the surface of earth where R is the radius of the earth .The time period of another satellite at a distance of 3.5R from the Centre of the earth is ….. hours.

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

A geostationary satellite is orbiting the earth at a height of 6R above the surface of the earth, where R is the radius of the earth. The time period of another satellite at a height of 2.5 R from the surface of the earth is …… hours.

A geostationary satellite is orbiting the earth at a height of 5R above the surface of the earth, R being the radius of the earth. The time period of another satellite in hours at a height of 2R form the surface of the earth is

A geostationary satellite is orbiting the earth at a height of 5R above the surface of the earth, 2R being the radius of the earth. The time period of another satellite in hours at a height of 2R form the surface of the earth is

A satellite orbits the earth at a height of 400 km, above the surface. How much energy must be expended to rocket the satellite out of the earth's gravitational influence ? Mass of the satellite=200 kg, mass of the earth= 6.0xx10^(24) kg, radius of the earth= 6.4xx10(6) m, G= 6.67xx10^(-11)Nm^(2)Kg^(-2) .

A satellite orbits the earth at a height of 400 km, above the surface. How much energy must be expended to rocket the satellite out of the earth's gravitational influence ? Mass of the satellite=200 kg, mass of the earth= 6.0xx10^(24) kg, radius of the earth= 6.4xx10(6) m, G= 6.67xx10^(-11)Nm^(2)Kg^(-2) .

A satellite of mass 1000 kg is supposed to orbit the earth at a height of 2000 km above the earth's surface. Find a. its speed in the orbit b . its kinetic energy. c . The potential energy of the earth-satellite system and d . its time period. Mass of the earth =6xx10^24kg .

A satellite of mass 1000 kg is supposed to orbit the earth at a height of 2000 km above the earth's surface. Find a). its speed in the orbit b). its kinetic energy. c). The potential energy of the earth satelilte system and d). its time period. Mass of the earth =6xx10^24kg .

A satellite is a at height of 25, 600 km from the surface of the earth. If its orbital speed is 3.536 km/s find its time period. (Radius of the earth = 6400 km)