`K.E.` of an orbiting satellite is `K`. The minimum additional `K.E.` required so that it goes to infinity is

The K.E. of a satellite is 10^(4)J . It's P.E. is

The K.E. of a satellite is 2MJ. Its total energy is

The ratio of the K.E. required to the given to the satellite to escape earth's gravitational field to the K.E. required to be given so that the satellite moves in a circular orbit just above earth atmosphere is

The ratio of the K.E. required to the given to the satellite to escape earth's gravitational field to the K.E. required to be given so that the satellite moves in a circular orbit just above earth atmosphere is

A satellite is orbiting close to the earth and has a kinetic energy K. The minimum extra kinetic energy required by it to just overcome the gravitation pull of the earth is

A satellite is orbiting close to the earth and has a kinetic energy K. The minimum extra kinetic energy required by it to just overcome the gravitation pull of the earth is

A satellite of mass m is in circular orbit of radius 3R_E about earth (mass of earth M_E , radius of earth R_E ). How much additional energy is required to transfer the satellite to an orbit of radius 9R_E ?