A lauching vehicle carrying an artificial satellite of mass `m` is set for launch on the surface of the earth of mass `M` and radius `R`. If the satellite intended to move in a circular orbit of radius `7R`, the minimum energy required to be spent by the launching vehicle on the satellite is

A launching vehicle carrying an artificial satellite of mass m is set for launch on the surface of the earth of mass M and radius R . If the satellite is intended to move in a circular orbit of radius 7R , the minimum energy . Required to be spent by the launching vehicle on the required to be spent by the launching vehicle on the satellite is (Gravitational constant =G)

At satellite of mass m is launched from the surface of a planet of mass M and radius R in a circular orbit at an altitude of 3R. K.E. of satellite at the time of launching is

The total energy of an artificial satellite of mass m revolving around the earth of mass M is ……….. The radius of the orbit of the satellite =r. [Fill in the blanks]

An artificial satellite of mass m is orbiting around the earth of mass M in an orbit of radius R, with a constant angular velocity. What is the angular momentum of a satellite ?

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

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?