A body of mass m is moving in a circular orbit of radius R about a planet of mass M. At some instant, it splits into two equal masses. The first mass moves in a circular orbit of radius `R/2`. And the other mass, in a circular orbit of radius `(3R)/(2)`. The difference between the final and initial total energies is :

A sayellite of mass m revolves in a circular orbit of radius R a round a planet of mass M. Its total energy E is :-

A sayellite of mass m revolves in a circular orbit of radius R a round a planet of mass M. Its total energy E is :-

A satellite of mass m revolves in a circular orbit of radius R a round a planet of mass M. Its total energy E is :-

An asteroid of mass M is moving , in a circular orbit of radius R about , the planet Taxed (Unknown Planet), which have mass M_(T) At some ,instant it split into 4 equal masses.,The first mass move in circular orbit of radius (R)/(11) , second mass move in the radius of (2R)/(11) ,third mass move ,in the radius (3R)/(11) and last one in (5R)/(11) .,Find the difference between the,initial and final total energies.

A satellite of mass 'm' is revolving in a circular orbit of radius 'r' around the earth of mass M. What is the total energy of the satellite?

A particle of charge q and mass m moves in a circular orbit of radius r with angular speed

The binding of a satellite of mass m in a orbit of radius r is

A satellite of mass M revolving in a circular orbit of radius r_(s) around the earth of mass M has a total energy E. then, its angular momentum will be

Two satellites , A and B , have masses m and 2m respectively . A is in a circular orbit of radius R , and B is in a circular orbit of radius 2R around the earth . The ratio of their energies , K_A/K_B is :

Two satellites , A and B , have masses m and 2m respectively . A is in a circular orbit of radius R , and B is in a circular orbit of radius 2R around the earth . The ratio of their energies , K_A/K_B is :