Home
Class 12
PHYSICS
A statellite is launched into a circular...

A statellite is launched into a circular orbit, `(R )/(4)` above the surface of the earth. The time period of revolution is `T=2pi(n)^(3//2)sqrt((R )/(g))`. Where R is the radius of the earth and g is the acceleration due to gravity. Then what is the value on n?

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem, we need to find the value of \( n \) in the given equation for the time period of a satellite in a circular orbit above the Earth's surface. ### Step-by-Step Solution: 1. **Understanding the Problem**: - The satellite is launched into a circular orbit at a height of \( \frac{R}{4} \) above the Earth's surface. - The radius of the Earth is denoted as \( R \). - The height \( h \) of the satellite from the Earth's surface is \( h = \frac{R}{4} \). - Therefore, the distance from the center of the Earth to the satellite (the orbital radius \( r \)) is: \[ r = R + h = R + \frac{R}{4} = \frac{5R}{4} \] 2. **Using the Time Period Formula**: - The time period \( T \) of a satellite in orbit is given by: \[ T = 2\pi \sqrt{\frac{r^3}{GM}} \] - Here, \( G \) is the gravitational constant and \( M \) is the mass of the Earth. 3. **Relating Gravitational Acceleration**: - The acceleration due to gravity \( g \) at the surface of the Earth is given by: \[ g = \frac{GM}{R^2} \] - Rearranging gives: \[ GM = gR^2 \] 4. **Substituting Values**: - Substitute \( r = \frac{5R}{4} \) into the time period formula: \[ T = 2\pi \sqrt{\frac{\left(\frac{5R}{4}\right)^3}{gR^2}} \] - Simplifying the expression: \[ T = 2\pi \sqrt{\frac{\frac{125R^3}{64}}{gR^2}} = 2\pi \sqrt{\frac{125R}{64g}} \] - This can be rewritten as: \[ T = 2\pi \cdot \frac{5}{8} \sqrt{\frac{R}{g}} = \frac{5\pi}{4} \sqrt{\frac{R}{g}} \] 5. **Comparing with Given Time Period**: - We are given the time period in the form: \[ T = 2\pi n^{3/2} \sqrt{\frac{R}{g}} \] - Set the two expressions for \( T \) equal to each other: \[ \frac{5\pi}{4} \sqrt{\frac{R}{g}} = 2\pi n^{3/2} \sqrt{\frac{R}{g}} \] 6. **Cancelling Common Terms**: - Cancel \( \sqrt{\frac{R}{g}} \) from both sides: \[ \frac{5}{4} = 2n^{3/2} \] 7. **Solving for \( n \)**: - Rearranging gives: \[ n^{3/2} = \frac{5}{8} \] - To find \( n \), raise both sides to the power of \( \frac{2}{3} \): \[ n = \left(\frac{5}{8}\right)^{\frac{2}{3}} \] 8. **Calculating \( n \)**: - Simplifying \( n \): \[ n = \frac{5^{\frac{2}{3}}}{8^{\frac{2}{3}}} = \frac{5^{\frac{2}{3}}}{(2^3)^{\frac{2}{3}}} = \frac{5^{\frac{2}{3}}}{2^2} = \frac{5^{\frac{2}{3}}}{4} \] ### Final Answer: The value of \( n \) is: \[ n = 1.25 \]
Promotional Banner

Similar Questions

Explore conceptually related problems

A satellite ils launched into a circular orbit 1600km above the surface of the earth. Find the period of revolution if the radius of the earth is R=6400km and the acceleration due to gravity is 9.8ms^(-2) . At what height from the ground should it be launched so that it may appear stationary over a point on the earth's equator?

If R is the radius of the earth and g the acceleration due to gravity on the earth's surface, the mean density of the earth is

Starting from the centre of the earth having radius R, the variation of g (acceleration due to gravity) is shown by

An earth satellite of mass m revolves in a circular orbit at a height h from the surface of the earth. R is the radius of the earth and g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by

An artificial satellite is moving in a circular orbit around the earth with a speed equal to half the magnitude of escape velocity from the surface of earth. R is the radius of earth and g is acceleration due to gravity at the surface of earth. (R=6400 km). The time period of revolution of satellite in the given orbit is

An artificial satellite is moving in circular orbit around the earth with speed equal to half the magnitude of escape velocity from the surface of earth. R is the radius of earth and g is acceleration due to gravity at the surface of earth (R = 6400km) Then the distance of satelite from the surface of earth is .

A particle of mass 'm' is raised from the surface of earth to a height h = 2R. Find work done by some external agent in the process. Here, R is the radius of earth and g the acceleration due to gravity on earth's surface.

The acceleration due to gravity at the surface of the earth is g . The acceleration due to gravity at a height (1)/(100) times the radius of the earth above the surface is close to :

A body is projected vertically upwards with speed sqrt(g R_(e )) from the surface of earth. What is the maximum height attained by the body ? [ R_(e ) is the radius of earth, g is acceleration due to gravity]

The acceleration due to gravity at a depth R//2 below the surface of the earth is