हिंदी

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.

Advertisements
Advertisements

प्रश्न

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.

संख्यात्मक
Advertisements

उत्तर

Given: M = 6.4 × 1024 kg, R = 3.4 × 106 m, m = 800 kg

To find: Energy required to remove the object from the surface of planet to infinity = B.E.

Formula: B.E. = `"GMm"/"R"`

Calculation: We know that,

G = 6.67 × 10–11 N m2/kg2

From formula,

B.E. = `(6.67 xx 10^-11 xx 6.4 xx 10^24 xx 800)/(3.4 xx 10^6)`

∴ B.E. =`(6.67 xx 6.4 xx 8)/3.4 xx 10^9`

∴ B.E. = 100.44 × 109 J

Energy required to remove the object from the surface of the planet is 1.004 × 1011 J.

shaalaa.com

Notes

The Answer given in the textbook is incorrect.

  क्या इस प्रश्न या उत्तर में कोई त्रुटि है?
अध्याय 5: Gravitation - Exercises [पृष्ठ ९९]

APPEARS IN

बालभारती Physics [English] Standard 11 Maharashtra State Board
अध्याय 5 Gravitation
Exercises | Q 4. (ix) | पृष्ठ ९९

संबंधित प्रश्न

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?


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.


The time period of an earth-satellite in circular orbit is independent of


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


Two satellites A and B move round the earth in the same orbit. The mass of B is twice the mass of A.


A Mars satellite moving in an orbit of radius 9.4 × 103 km takes 27540 s to complete one revolution. Calculate the mass of Mars.


Answer the following question.

What do you mean by geostationary satellite?


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


Draw a labelled diagram to show different trajectories of a satellite depending upon the tangential projection speed.


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


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


Answer the following question in detail.

Two satellites A and B are revolving round a planet. Their periods of revolution are 1 hour and 8 hour respectively. The radius of orbit of satellite B is 4 × 104 km. Find radius of orbit of satellite A.


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.


Which of the following statements is CORRECT in respect of a geostationary satellite?


The kinetic energy of a revolving satellite (mass m) at a height equal to thrice the radius of the earth (R) is ______.


If a body weighing 40 kg is taken inside the earth to a depth to radius of the earth, then `1/8`th the weight of the body at that point is ______.


If the Earth-Sun distance is held constant and the mass of the Sun is doubled, then the period of revolution of the earth around the Sun will change to ____________.


If a body weighing 40 kg-wt is taken inside the earth to a depth to `1/2` th radius of the earth, then the weight of the body at that point is ____________.


A satellite of mass 'm', revolving round the earth of radius 'r' has kinetic energy (E). Its angular momentum is ______.


A satellite is to revolve round the earth in a circle of radius 9600 km. The speed with which this satellite be projected into an orbit, will be ______.


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


A satellite revolves around a planet very close to its surface. By what maximum factor can its kinetic energy be increased suddenly, such that it revolves in orbit in the same way?


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)


Two satellites of same mass are orbiting round the earth at heights of r1 and r2 from the centre of earth. Their potential energies are in the ratio of ______.


What is the approximate period of revolution for the Moon, Earth's only natural satellite?


Which application is mainly associated with polar satellites?


Share
Notifications

Englishहिंदीमराठी


      Forgot password?
Use app×