Advertisements
Advertisements
Question
What is the true weight of an object in a geostationary satellite that weighed exactly 10.0 N at the north pole?
Advertisements
Solution
For a geostationary satellite, we have:
R = 6.4 × 103 km
h = 3.6 × 103 km
Given: mg = 10 N
The true weight of the object in the geostationary satellite is given by
\[\text { mg' = mg }- \frac{R^2}{\left( R + h \right)^2}\]
\[ = 10 - \frac{\left( 6400 \times {10}^3 \right)^2}{\left( 6400 \times {10}^3 + 3600 \times {10}^3 \right)}\]
\[ = 10 - \left[ \frac{\left( 64 \times {10}^5 \right)^2}{\left( 6 . 4 \times {10}^6 + 36 \times {10}^5 \right)} \right]\]
\[ = 10 - \left[ \frac{4096 \times {10}^{10}}{\left( 42 . 4 \right)^2 \times {10}^{12}} \right]\]
\[ = \frac{4096}{17980} = 0 . 227 N\]
APPEARS IN
RELATED QUESTIONS
Suppose there existed a planet that went around the sun twice as fast as the earth.What would be its orbital size as compared to that of the earth?
As the earth rotates about its axis, a person living in his house at the equator goes in a circular orbit of radius equal to the radius of the earth. Why does he/she not feel weightless as a satellite passenger does?
A satellite is orbiting the earth close to its surface. A particle is to be projected from the satellite to just escape from the earth. The escape speed from the earth is ve. Its speed with respect to the satellite
The radius of a planet is R1 and a satellite revolves round it in a circle of radius R2. The time period of revolution is T. Find the acceleration due to the gravitation of the planet at its surface.
Answer the following question.
Define the binding energy of a satellite.
State the conditions for various possible orbits of satellite depending upon the horizontal/tangential speed of projection.
Derive an expression for the critical velocity of a satellite.
Solve the following problem.
Calculate the speed of a satellite in an orbit at a height of 1000 km from the Earth’s surface.
(ME = 5.98 × 1024 kg, R = 6.4 × 106 m)
A planet has mass 6.4 × 1024 kg and radius 3.4 × 106 m. Calculate the energy required to remove an object of mass 800 kg from the surface of the planet to infinity.
A body weighs 5.6 kg wt on the surface of the Earth. How much will be its weight on a planet whose mass is 7 times the mass of the Earth and radius twice that of the Earth’s radius?
The ratio of energy required to raise a satellite of mass 'm' to a height 'h' above the earth's surface of that required to put it into the orbit at same height is ______.
[R = radius of the earth]
An aircraft is moving with uniform velocity 150 m/s in the space. If all the forces acting on it are balanced, then it will ______.
Reason of weightlessness in a satellite is ____________.
A geostationary satellite is orbiting the earth at the height of 6R above the surface of earth. R being radius of earth. The time period of another satellite at a height of 2.5 R from the surface of earth is ____________.
Assuming that the earth is revolving around the sun in circular orbit of radius 'R', the angular momentum is directly proportional to rn. The value of 'n' is ______.
In the case of earth, mean radius is 'R', acceleration due to gravity on the surface is 'g', angular speed about its own axis is 'ω'. What will be the radius of the orbit of a geostationary satellite?
Show the nature of the following graph for a satellite orbiting the earth.
- KE vs orbital radius R
- PE vs orbital radius R
- TE vs orbital radius R.
A satellite is revolving around a planet in a circular orbit close to its surface and ρ is the mean density and R is the radius of the planet, then the period of ______.
(G = universal constant of gravitation)
What is the typical altitude range for a polar satellite's orbit?
