Explanation:
It is given that,
Radius of unknown planet, [tex]r=2\times 10^7\ m[/tex]
The magnitude of the gravitational force on the satellite from the planet is F = 80 N, it means,
[tex]\dfrac{GmM}{r^2}=80[/tex]
The gravitational force acting on the satellite is balanced by the centripetal force as :
(a) Let E is the is the kinetic energy of the satellite in this orbit.
[tex]\dfrac{GmM}{r^2}=\dfrac{mv^2}{r}[/tex]
[tex]mv^2=\dfrac{GmM}{r^2}\times r[/tex]
[tex]mv^2=80\times 2\times 10^7[/tex]
[tex]mv^2=1.6\times 10^9\ kg-m^2/s^2[/tex]
Multiply both sides of above equation by 1/2.
[tex]\dfrac{1}{2}mv^2=\dfrac{1}{2}\times 1.6\times 10^9\ kg-m^2/s^2[/tex]
[tex]\dfrac{1}{2}mv^2=8\times 10^8\ J[/tex]
So, [tex]E=8\times 10^8\ J[/tex]'
(b) Let F' is the force if the orbit radius were increased to, [tex]r'=3\times 10^7\ m[/tex]
The relation between the force and distance is,
[tex]\dfrac{F'}{F}=(\dfrac{r}{r'})^2[/tex]
[tex]\dfrac{F'}{80}=(\dfrac{2\times 10^7}{3\times 10^7})^2[/tex]
F' = 35.55 N
or
F' = 36 N
Hence, this is the required solution.