Kepler, around 1600, upon his meticulous observations and measurements, had established a remarkable relationship between the revolution period T of a planet around the Sun, and the distance R of it to the Sun, as T2-R3. Show, how Newton about a century later, could, not only derive this relationship, as (with the familiar notation), T2=[(4π2/GM]R3, but also, could fix Kepler’s “proportionality constant”, thusly becoming 4π2/GM. The quantity G, is the gravitation constant, and M is the mass of the Sun.
b) ( p) We can well apply Kepler’s Law not only to the System made of the Sun and the planets revolving around the Sun, but also to any celestial system, and in particular to Earth and the Moon revolving around Earth. Thus, show that the square of the period of rotation TM of the Moon around Earth, can be expressed as TM2=[(4π2/gRE2]RM3, where g is Earth’s acceleration, we defined in Question 1, and RM, is the distance from Earth to the Moon.
c) () The period TM, is, as we well know, about 1 month. Find then RM, taking RE to be 6000 km. Make sure that, you use coherent units. As you see one can determine the distance between Earth and the Moon,from where he sits.
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