Answer :
Answer:
A. 0.25
Explanation:
G = Gravitational constant
M = Mass of Earth
m = Mass of space station = Mass of satellite
r = Distance between Earth and object
Centripetal force on Space Station
[tex]F_{ss}=\frac{GMm}{r^2}[/tex]
Centripetal force on satellite
[tex]F_{s}=\frac{GMm}{(2r)^2}\\\Rightarrow F_{ss}=\frac{GMm}{4r^2}[/tex]
Divinding the forces we get
[tex]\frac{F_s}{F_{ss}}=\frac{\frac{GMm}{4r^2}}{\frac{GMm}{r^2}}\\\Rightarrow \frac{F_s}{F_{ss}}=\frac{1}{4}=0.25[/tex]
The ratio of centripetal force acting on the satellite compared to that acting on the International Space Station is 0.25