Advertisements
Advertisements
प्रश्न
What is the true weight of an object in a geostationary satellite that weighed exactly 10.0 N at the north pole?
Advertisements
उत्तर
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
संबंधित प्रश्न
A nut becomes loose and gets detached from a satellite revolving around the earth. Will it land on the earth? If yes, where will it land? If no, how can an astronaut make it land on the earth?
Consider earth satellites in circular orbits. A geostationary satellite must be at a height of about 36000 km from the earth's surface. Will any satellite moving at this height be a geostationary satellite? Will any satellite moving at this height have a time period of 24 hours?
A spacecraft consumes more fuel in going from the earth to the moon than it takes for a return trip. Comment on this statement.
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) is kinetic energy, (c) the potential energy of the earth-satellite system and (d) its time period. Mass of the earth = 6 × 1024kg.
Answer the following question.
Define the binding energy of a satellite.
Derive an expression for the critical velocity of a satellite.
Draw a labelled diagram to show different trajectories of a satellite depending upon the tangential projection speed.
Answer the following question in detail.
Obtain an expression for the critical velocity of an orbiting satellite. On what factors does it depend?
Solve the following problem.
Calculate the value of acceleration due to gravity on the surface of Mars if the radius of Mars = 3.4 × 103 km and its mass is 6.4 × 1023 kg.
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.
Solve the following problem.
What is the gravitational potential due to the Earth at a point which is at a height of 2RE above the surface of the Earth?
(Mass of the Earth is 6 × 1024 kg, radius of the Earth = 6400 km and G = 6.67 × 10–11 N m2 kg–2)
Which of the following statements is CORRECT in respect of a geostationary satellite?
There is no atmosphere on moon because ____________.
Two satellites of masses m1 and m2 (m1 > m2) are revolving round the earth in circular orbit of radii r1 and r2 (r1 > r2) respectively. Which of the following statements is true regarding their speeds v1 and v2?
A satellite is revolving in a circular orbit around the earth has total energy 'E'. Its potential energy in that orbit is ______.
Satellites orbiting the earth have finite life and sometimes debris of satellites fall to the earth. This is because ______.
A satellite is revolving in a circular orbit at a height 'h' above the surface of the earth of radius 'R'. The speed of the satellite in its orbit is one-fourth the escape velocity from the surface of the earth. The relation between 'h' and 'R' is ______.
What is the approximate period of revolution for the Moon, Earth's only natural satellite?
Artificial satellites are launched for all the following purposes EXCEPT ______.
Which application is mainly associated with polar satellites?
