Home
Class 11
PHYSICS
A sky laboratory of mass 2 xx 10^(3) kg ...

A sky laboratory of mass `2 xx 10^(3) kg` has to be lifted from one circular orbit of radius `2R` into another circular orbit of radius `3R`. Calculate the minimum energy required if the radius of earth is `R= 6.37 xx 10^(6) m` and `g= 9.8 ms^(-2)`

Text Solution

Verified by Experts

The correct Answer is:
`1.04xx10^(10)J`

Total energy of sky laboratory `E=-(GMm)/(2r)`
`E_(1)=-(GMm)/(2(2R))` and `E_(2) =-(GMm)/(2(3R))`
Therefore the energy required
`/_\E=E_(2)-E_(1)=GMm(1/(4R)-1/(6R))=(GMm)/(12R)`
`((R^(2)g)m)/(12R)=(mgR)/12=1.04xx10^(10)J`
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    CENGAGE PHYSICS|Exercise Single Correct|122 Videos
  • GRAVITATION

    CENGAGE PHYSICS|Exercise Multiple Correct|24 Videos
  • GRAVITATION

    CENGAGE PHYSICS|Exercise Exercise 6.4|16 Videos
  • FLUID MECHANICS

    CENGAGE PHYSICS|Exercise INTEGER_TYPE|1 Videos
  • KINEMATICS-1

    CENGAGE PHYSICS|Exercise Integer|9 Videos

Similar Questions

Explore conceptually related problems

A satellite of mass 2xx10^(3)kg has to be shifted from an orbit of radius 2R to another of radius 3R, where R is the radius of the earth. Calculate the minimum energy required. Take mass of earth =6xx10^(24)kg , radius of earth =6.4xx10^(6)m .

A satellite revolves around the earth of radius R in a circular orbit of radius 3R. The percentage increase in energy required to lift it to an orbit of radius 5R i

A sky lab of mass 2 xx 10^(3)kg is first lauched from the surface of earth in a circular orbit of radius 2R and them it is shifted from this circular orbit to another circular orbit of radius 3R . Calculate the energy required (a) to place the lab in the first orbit, (b) to shift the lab from first orbit to the second orbit. (R = 6400 km , g = 10 m//s^(2))

The time period of a satellite in a circular orbit of radius R is T. The period of another satellite in a circular orbit of radius 9R is :

In order to shift a body of mass m from a circular orbit of radius 3R to a higher orbit of radius 5R around the earth, the work done is

A skylab of mass m kg is first launched from the surface of the earth in a circular orbit of radius 2R (from the centre of the earth) and then it is shifted from this circular orbit to another circular orbit of radius 3R . The minimum energy required to place the lab in the first orbit and to shift the lab from first orbit to the second orbit are

A satallite of mass m , initally at rest on the earth, is launched into a circular orbit at a height equal to the the radius of the earth. The minimum energy required is

If a planet of mass m is revolving around the sun in a circular orbit of radius r with time period, T then mass of the sun is