How Long Does It Take the Second Satellite to Orbit Jupiter?

AI Thread Summary
The discussion revolves around calculating the orbital period of a second satellite orbiting Jupiter, which has an orbital radius four times that of the first satellite. The first satellite completes one revolution every 16 hours. Participants emphasize the importance of showing initial problem-solving efforts before receiving assistance. Key formulas mentioned include those for centripetal acceleration and angular velocity, which are essential for determining the second satellite's orbital period. The conversation highlights the need for a solid understanding of gravitational physics to solve the problem effectively.
trainumc
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i am comlpetely stuck on this problem

Two satellites are in circular orbits around Jupiter. One, with orbital radius r, makes one revolution every 16 h. The other satellite has orbital radius 4.0r. How long does the second satellite take to make one revolution around Jupiter?

any help please?
 
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trainumc said:
i am comlpetely stuck on this problem

Two satellites are in circular orbits around Jupiter. One, with orbital radius r, makes one revolution every 16 h. The other satellite has orbital radius 4.0r. How long does the second satellite take to make one revolution around Jupiter?

any help please?
Welcome to Physics Forums.

We we certainly help you, but before we do you are required to show some effort in solving the problem yourself, either by providing a attempted solution or at the very least detailing your thoughts.

The homework template is there for a reason. Please use it.
 
well i don't know how to find the height but for the acceleration i know if

G= 6.67*10^-11
M= 5.97*10^24

then V=sqrt((GM/r)

but my solutions don't seem to be working
 
You're on the right lines, but not quite there yet. I'll offer you a few hints in the right direction.

a_c = \omega^2 r

\omega = \frac{2\pi}{T}

Where T is the orbital period.
 
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