<span>F = GMm / r^2. ( When at the surface). </span> <span>G = Universal gravitational constant, G = 6.67 * 10 ^ -11 Nm^2 / kg^2. M = Mass of Moon m = Mass of Satellite r = distance apart, between centers = in this case it is the distance from Moon to the Satellite.</span>
Recall: F = mg.
mg = <span>GMm / r^2 g = GM / r^2.........................(i). When at surface.
Note when the satellite is at a distance 2 times the radius of the moon. Therefore, the distance between centers = 2r + r = 3r. Note, when need to add radius of the moon, because we are measuring from center of the satellite to center of the moon.
From (i)</span> <span><span>g = GM / (3r)^2</span>. The distance r is replaced with 3r
g = GM / 9r^2 = (1/9) * GM / r^2
Therefore gravity on the satellite is (1/9) times that on the Moon. </span>
The orbit is a circle whose radius is 3 times the radius of the surface (both measured from the center of the moon). So the acceleration due to gravity at the orbital altitude is
1/3² = 1/9 = <em>11.1% of its value</em> on the surface.