This is a discrete question which I'm confused about because of possible missing information. Let's say there are two satellites, A and B. Satellite A is resting on the surface of Earth and satellite B is orbiting Earth from an altitude of R, directly over Satellite A. Satellite B is twice the mass of Satellite A. The question then asks for the ratio of Earth's gravitational force on A over its force on B.
A) 1/4
B) 1/2
C) 1
D) 2
I was thinking that I could solve this problem by using F=GmM/r^2. I could plug in r = (R) for F(B) and r = (radius of earth) for F(A). But I wouldn't know exactly by how much "R" and "radius of earth" differ.
Apparently, to solve this, you set up the ratio F(A)/F(B) as I had thought about, but here are their values according to the text:
F(A) = GMm(a)/R^2
F(B) = GMm(b)/(2R)^2
The question stem clearly says that the altitude of B from the surface of Earth is R. Why is R plugged into F(a), and 2R plugged into F(b)?
A) 1/4
B) 1/2
C) 1
D) 2
I was thinking that I could solve this problem by using F=GmM/r^2. I could plug in r = (R) for F(B) and r = (radius of earth) for F(A). But I wouldn't know exactly by how much "R" and "radius of earth" differ.
Apparently, to solve this, you set up the ratio F(A)/F(B) as I had thought about, but here are their values according to the text:
F(A) = GMm(a)/R^2
F(B) = GMm(b)/(2R)^2
The question stem clearly says that the altitude of B from the surface of Earth is R. Why is R plugged into F(a), and 2R plugged into F(b)?