Respuesta :
Let
M = the mass of the planet
n = the mass of the satellite.
r = the radius of the planet
When the satellite is at a distance r from the surface of the planet, the distance between the centers of the two masses is 2r.
The gravitational force between them is
[tex]f_{0} = \frac{GMm}{(2r)^{2}} = \frac{1}{4} ( \frac{GMm}{r^{2}} )[/tex]
where
G = the gravitational constant.
When the satellite is on the surface of the planet, the distance between the two masses is r.
The gravitational force between them is
[tex]f_{4} = \frac{GMm}{r^{2}} =4f_{0}[/tex]
Answer: [tex]f_{4} = 4f_{0}[/tex]
M = the mass of the planet
n = the mass of the satellite.
r = the radius of the planet
When the satellite is at a distance r from the surface of the planet, the distance between the centers of the two masses is 2r.
The gravitational force between them is
[tex]f_{0} = \frac{GMm}{(2r)^{2}} = \frac{1}{4} ( \frac{GMm}{r^{2}} )[/tex]
where
G = the gravitational constant.
When the satellite is on the surface of the planet, the distance between the two masses is r.
The gravitational force between them is
[tex]f_{4} = \frac{GMm}{r^{2}} =4f_{0}[/tex]
Answer: [tex]f_{4} = 4f_{0}[/tex]
f4 is 4 times larger than f0
The force of gravity between two masses is
F = G M1M2/r^2
where
F = Force
G = Gravitational constant
M1 = Mass of object 1
M2 = Mass of object 2
r = distance between the center of masses of the objects.
So in the first case, the satellite is at an altitude of r above the surface. But it's really at a distance of 2r from the center of mass of the planet. And in the second case, the situation is that it's at distance r from the center of mass of the planet. So we have:
f0 = G M1M2/((2r)^2) = G M1M2/(4r^2)
and
f4 = G M1M2/r^2
Let's divide f4 by f0
(G M1M2/r^2) / G M1M2/(4r^2)
= (G M1M2/r^2) * (4r^2)/(G M1M2)
= (1/r^2) * (4r^2)/1
= (4r^2)/r^2
= 4/1
= 4
So f4 = f0 * 4