A spaceship is launched into a circular orbit close to the earth's surface . What additional velocity has now to be imparted to the spaceship in the orbit to overcome the gravitational pull. Radius of earth `= 6400 km`, `g = 9.8m//s^(2)`.

A spaceship is launced into a circular orbit close to the earth's aurface . What additional velocity has now to be imparted to the spaceship in the orbit to overcome the gravitational pull. Radius of earth = 6400 km , g = 9.8m//s^(2) .

A satellite is launched into a circular orbit close to the earth's surface. What additional velocity has new to be imparted to the satellite in the orbit to overcome the gravitational pull ?

A spaceship is launched into a circular orbit close to the Earth's surface. What additional velocity has to be imparted to the spaceship to overcome the gravitational pull?

A space-ship is launched into a circular orbit close to the Earth,s surface. What additional speed should now be imparted to the spaceship so that it overcome the gravitational pull of the Earth. Take kinetic energy of the space-ship, K = total energy of space-ship = (GMm)/(2R) where m = mass of space-ship, M= mass of the earth and R = radius of the earth.

A spaceship is launched in to a circular orbit of radius R close to surface of earth. The additional velocity to be imparted to the spaceship in the orbit to overcome the earth's gravitational pull is ( g =acceleration due to gravity)

A spacecraft is launched in a circular orbit very close to earth. What additional velocity should be given to the spacecraft so that it might escape the earth's gravitational pull.

A satellite orbiting close to the surface of earth does not fall down becouse the gravitational pull of earth

A projectile is launched vertically from earth's surface with an inittial velocity of 10 km/s. Calculate the height it will reach above the earth's surface. Take, Radius of earth = 6,400 km g = 9.8 m//s^(2)

If v_(0) orbital velocity of a surface to a circular orbital close in the earth's surface and v_(1) scape velocity from earth then relation between the two is