Advertisements
Advertisements
Question
A body stretches a spring by a particular length at the earth's surface at the equator. At what height above the south pole will it stretch the same spring by the same length? Assume the earth to be spherical.
Advertisements
Solution
At the equator, g' = g − ω2R ...(i)
Let h be the height above the South Pole where the body stretch the spring by the same length.
The acceleration due to gravity at this point is \[g' = g\left( 1 - \frac{2h}{R} \right)\]
Weight of the body at the equator = weight of the body at height h above the South Pole
\[\therefore g - \omega^2 r = g\left( 1 - \left( \frac{2h}{R} \right) \right)\]
\[ \Rightarrow 1 - \frac{\omega^2 R}{2g} = 1 - \frac{2h}{R}\]
\[ \Rightarrow h = \frac{\omega^2 R^2}{2g}\]
\[ = \frac{\left( 7 . 3 \times {10}^{- 5} \right)^2 \times \left( 6400 \times {10}^{- 3} \right)^2}{2 \times 9 . 81}\]
\[ = \frac{\left( 7 . 3 \right)^2 \times \left( 64 \right)^2}{19 . 62}\]
\[ = 11125 \text{ m }= 10 \text{ km} \left( \text { approx }. \right)\]
APPEARS IN
RELATED QUESTIONS
Is it necessary for the plane of the orbit of a satellite to pass through the centre of the earth?
No part of India is situated on the equator. Is it possible to have a geostationary satellite which always remains over New Delhi?
Answer the following question.
What is periodic time of a geostationary satellite?
Answer the following question in detail.
Why an astronaut in an orbiting satellite has a feeling of weightlessness?
Answer the following question in detail.
Obtain an expression for the binding energy of a satellite revolving around the Earth at a certain altitude.
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)
Solve the following problem.
Calculate the value of the universal gravitational constant from the given data. Mass of the Earth = 6 × 1024 kg, Radius of the Earth = 6400 km, and the acceleration due to gravity on the surface = 9.8 m/s2.
What is the minimum energy required to launch a satellite of mass 'm' from the surface of the earth of mass 'M' and radius 'R' at an altitude 2R?
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?
Two satellites of masses m and 4m orbit the earth in circular orbits of radii 8r and r respectively. The ratio of their orbital speeds is ____________.
Out of following, the only correct statement about satellites is ____________.
The ratio of energy required to raise a satellite to a height `(2R)/3` above earth's surface to that required to put it into the orbit at the same height is ______.
R = radius of the earth
A satellite of mass 'm', revolving round the earth of radius 'r' has kinetic energy (E). Its angular momentum is ______.
The period of revolution of a satellite is ______.
Is it possibe for a body to have inertia but no weight?
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.
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 of the following is the only natural satellite of the Earth?
