The formula to find the period of orbit of a satellite around a planet is T^2=(4pi^2/GM)r^3 where r is the orbit's mean radius, M is the mass of the planet, and G is the universal gravitational constant. if you are given all the values except r, how do you rewrite the formula to solve for r?
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Question

The formula to find the period of orbit of a satellite around a planet is T^2=(4pi^2/GM)r^3 where r is the orbit's mean radius, M is the mass of the planet, and G is the universal gravitational constant. if you are given all the values except r, how do you rewrite the formula to solve for r?
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ooxbrittanyxoo · Answer

A) $$r=\sqrt[3]{GMT \div4\pi ^{2}}$$
B) $$r=T \div2\pi \sqrt[3]{GM}$$
C) $$r=\sqrt[3]{GMT ^{2}\div4\pi ^{2}}$$
D) $$r=\sqrt[3]{GMT ^{2}\div4\pi}$$

syedmohammed98 · Answer

http://openstudy.com/study#/updates/55b26bffe4b0ce10565f633c there ya go

ooxbrittanyxoo · Answer

thnx lots