The value of gravitational accelerationg at a height h above the earth's surface is then (R = radius of earth)

The value of gravitational accelerationg at a height h above the earth's surface is 0ne forth the value of gravitational acceleration at surface ,then (R = radius of earth)

The value of gravitational acceleration 'g' at a height 'h' above the earth's surface is (g)/(4) , then (R = __________ ) (where R = radius of the earth)

The value of gravitational acceleration 'g' at a height 'h' above the earth's surface is (g)/(4) , then (R = __________ ) (where R = radius of the earth)

If g_(h) is the acceleration due to gravity at a height h above the earth's surface and R is the radius of the earth then, the critical velocity of a satellite revolving round the earth in a circular orbit at a height h is equal to

If h_(T) and h_(R) are the height of the transmitting and receiving antennas above the earth's surface and R is the radius of earth, then distance between the transmitting and receiving antenna is

A geostationary satellite is at a height h above the surface of earth. If earth radius is R -

The gravitational potential energy of body of mass 'm' at the earth's surface - mgR_(e) . Its gravitational potential energy at a height R_(e) from the earth's surface will be (here R_(e) is the radius of the earth)

The gravitational potential energy of a body of mass m at the earth's surface is mgR_e . Its gravitational potential energy at a height R_e from the earth's surface will be ..... (Here R_e is the radius of earth)

The gravitational potential energy of a body of mass ‘ m ’ at the earth’s surface -mgR_(e) . Its gravitational potential energy at a height R_(e) from the earth’s surface will be (Here R_(e) is the radius of the earth)

The gravitational potential energy of body of mass 'm' at the earth's surface mgR_(e) . Its gravitational potential energy at a height R_(e) fromt the earth's surface will be (here R_(e) is the radius of the earth)