Home
Class 12
PHYSICS
Two planets of mass M and 16M of radius ...


Two planets of mass `M` and `16M` of radius `a` and `2a` respectively, are at distance `10a`. Find minimum speed of a particle of mass m at surface of smaller planet so that it can reached from smaller planet to larger planet.

A

`sqrt((5/9) (GM)/a)`

B

`sqrt((4/9) (GM)/a)`

C

`sqrt((3/9) (GM)/a)`

D

`sqrt((2/9) (GM)/a)`

Text Solution

Verified by Experts

The correct Answer is:
A
Doubtnut Promotions Banner Mobile Dark
|

Topper's Solved these Questions

  • JEE MAIN 2021

    JEE MAINS PREVIOUS YEAR|Exercise PHYSICS SECTION B|30 Videos

Similar Questions

Explore conceptually related problems

Two planets have masses M and 16 M and their radii are a and 2a, respectively. The separation between the centres of the planets is 10a. A body of mass m is fired trom the surface of the larger planet towards the samller planet along the line joining their centres. For the body to be able to reach at the surface of smaller planet, the minimum firing speed needed is :

A solid spherical planet of mass 2m and radius 'R' has a very small tunnel along its diameter. A small cosmic particle of mass m is at a distance 2R from the centre of the planet as shown. Both are initially at rest, and due to gravitational attraction, both start moving toward each other. After some time, the cosmic particle passes through the centre of the planet. (Assume the planet and the cosmic particle are isolated from other planets)

Knowledge Check

  • What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 2R?

    A
    `(5GmM)/(6R)`
    B
    `(2GmM)/(3R)`
    C
    `(GmM)/(2R)`
    D
    `(GmM)/(2R)`
  • What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 2R?

    A
    `( 5 G m M )/( 6 R)`
    B
    `( 2 G m M )/( 3 R)`
    C
    `( G m M )/( 2R)`
    D
    `( G m M )/( 3 R)`
  • What is the minimum energy required to launch a satellite of mass m from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 3R ?

    A
    `(7"GmM")/(8R)`
    B
    `(2"GmM")/(3R)`
    C
    `("GmM")/(2R)`
    D
    `("GMm")/(2R)`
  • Similar Questions

    Explore conceptually related problems

    Mass and radius of a planet are two times the value of earth. What is the value of escape velocity from the surface of this planet?

    A small asteroid is approaching a planet of mass M and radius R from a large distance. Initially its velocity (u) is along a tangent to the surface of the planet. It fall on the surface making an angle of 30^(2) with the vertical. Calculate u.

    The earth is a homogeneous sphere of mass M and radius R. There is another spherical planet of mass M and radius R whose density changes with distance r from the centre as p=p_(0)r. (a) Find the ratio of acceleration due to gravity on the surface of the earth and that on the surface of the planet. (b) Find p_(0).

    A spherical planet far out in space has a mass M_0 and diameter D_0 . A particle of mass m falling freely near the surface of this planet will experience acceleration due to gravity equal to

    Planet A has a mass and radius twice that of Planet B. The escape velocity from Planet A is