A satellite is revolving round the earth (mass `M_(e)`) in a circular orbit of radius `a` with velocity `V_(0)` A particle of mass `m` is projected from the satellite in forward direction with relative velocity `v[sqrt((5)/(4))-1]V_(0)`. During subsequent motion of particle.

A satellite is revolving round the earth in a circular orbit of radius r and velocity upsilon_(0) . A particle is projected from the satellite in forward direction with realative velocity upsilon = (sqrt(5//4) - 1) upsilon_(0) . Calculate its minimum and maximum distances from earth's centre during subsequent motion of the particle.

A satellite is revolving round the earth in a circular orbit of radius r and velocity upsilon_(0) . A particle is projected from the satellite in forward direction with realative velocity upsilon = (sqrt(5//4) - 1) upsilon_(0) . Calculate its minimum and maximum distances from earth's centre during subsequent motion of the particle.

A satellite is orbiting around the earth in a circular orbit of radius r . A particle of mass m is projected from the satellite in a forward direction with a velocity v = 2//3 times the orbital velocity (this velocity is given w.r.t. earth). During subsequent motion of the particle, its minimum distance from the centre of earth is

A satellite is orbiting around the earth in a circular orbit of radius r . A particle of mass m is projected from the satellite in a forward direction with a velocity v = 2//3 times the orbital velocity (this velocity is given w.r.t. earth). During subsequent motion of the particle, its minimum distance from the centre of earth is

A satellite is orbiting around earth in a circular orbit of radius r . A particle of mass m is projected from satellite in forward direction with velocity v=sqrt(2/3) times orbital velocity (this velocity is with respect to the earth). During subsequent motion of the particle, its minimum distance from the centre of earth is