English

State the conditions for various possible orbits of satellite depending upon the horizontal/tangential speed of projection. - Physics

Advertisements
Advertisements

Question

State the conditions for various possible orbits of satellite depending upon the horizontal/tangential speed of projection.

Short Answer
Advertisements

Solution

The path of the satellite depends upon the value of the horizontal speed of projection vh relative to critical velocity vc and escape velocity ve.

Case (I) vh < vc:

The orbit of the satellite is an ellipse with a point of projection as the apogee and Earth at one of the foci. During this elliptical path, if the satellite passes through the Earth’s atmosphere, it experiences a nonconservative force of air resistance. As a result, it loses energy and spirals down to the Earth.

Case (II) vh = vc:

The satellite moves in a stable circular orbit around the Earth.

Case (III) vc < v< ve:

The satellite moves in an elliptical orbit around the Earth with the point of projection as perigee.

Case (IV) vh = ve:

The satellite travels along the parabolic path and never returns to the point of projection. Its speed will be zero at infinity.

Case (V) vh > ve:

The satellite escapes from the gravitational influence of Earth traversing a hyperbolic path.

shaalaa.com
  Is there an error in this question or solution?
Chapter 5: Gravitation - Exercises [Page 97]

APPEARS IN

Balbharati Physics [English] Standard 11 Maharashtra State Board
Chapter 5 Gravitation
Exercises | Q 2. (xv) | Page 97

RELATED QUESTIONS

Is it necessary for the plane of the orbit of a satellite to pass through the centre of 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?


At what rate should the earth rotate so that the apparent g at the equator becomes zero? What will be the length of the day in this situation?


Find the minimum colatitude which can directly receive a signal from a geostationary satellite.


Answer the following question.

Why is a minimum two-stage rocket necessary for launching of a satellite?


Answer the following question in detail.

State any four applications of a communication satellite.


Derive an expression for the binding energy of a body at rest on the Earth’s surface of a satellite.


Answer the following question in detail.

What is a critical velocity?


Describe how an artificial satellite using a two-stage rocket is launched in an orbit around the Earth.


Calculate the kinetic energy, potential energy, total energy and binding energy of an artificial satellite of mass 2000 kg orbiting at a height of 3600 km above the surface of the Earth.
Given: G = 6.67 × 10-11 Nm2/kg2
R = 6400 km, M = 6 × 1024 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.

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.


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]


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 ____________.


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 is revolving in a circular orbit around the earth has total energy 'E'. Its potential energy in that orbit is ______.


A geostationary satellite is orbiting the earth at a height 6R above the surface of the earth, where R is the radius of the earth. This time period of another satellite at a height (2.5 R) from the surface of the earth is ______.


Show the nature of the following graph for a satellite orbiting the earth. 

  1. KE vs orbital radius R
  2. PE vs orbital radius R
  3. TE vs orbital radius R.

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 earth. If the satellite is stopped in its orbit and allowed to fall freely onto the earth, the speed with which it hits the surface ______ km/s.

[g = 9.8 ms-2 and Re = 6400 km]


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 ______.


The ratio of binding energy of a satellite at rest on earth's surface to the binding energy of a satellite of same mass revolving around the earth at a height h above the earth's surface is ______ (R = radius of the earth).


Which of the following is an example of a communication (geostationary) satellite launched by India?


Artificial satellites are launched for all the following purposes EXCEPT:


Share
Notifications

Englishहिंदीमराठी


      Forgot password?
Use app×