1. An artificial satellite circles the earth in a circular orbit at a location where the acceleration due to gravity is 9.0ms-2. Determine the orbital period of the satellite.
2. A satellite of Jupiter has an orbital period of 1.77 days and an orbital radius of . Determine the mass of Jupiter.
Let's write a given constants
G = 6.67 * 10-11 ["\\frac{m^3*s^2}{kg}"] and "M_{earth}" = 6 * 1024 kg a = 9["\\frac{m}{s^2}"]
First, we compute R from a = "\\frac{GM}{R^2}", We find R = "\\sqrt{\\frac{GM}{a}}"
Second we compute v from a = "\\frac{v^2}{R}" , which gives v = "\\sqrt{aR}" = "\\sqrt[4]{GMa}"
Finally, we compute T from this v = "\\frac{2\\pi R}{T}"
T = "\\frac{2\\pi R}{v} = 2\\pi * \\sqrt{GMa} * \\frac{1}{\\sqrt[4]{GMa}} = 2\\pi * \\sqrt[4]{\\frac{GM}{a^3}}"
= 6.28 * "\\sqrt[4]{\\frac{6.67 * 10^{-11} * 6 * 10^{24}}{27}}" = 12322[s] = 3.42[hour]
"T = \\frac{2\\pi R}{v} = \\frac{2\\pi R}{\\sqrt{aR}} = \\frac{2\\pi R}{\\sqrt{\\frac{GM}{R^2}R}} = \\frac{2\\pi R\\sqrt{R}}{\\sqrt{GM}} = \\frac{6.28 * 7 * 10^7 * \\sqrt{7 * 10^7}}{\\sqrt{6.67*10^{-11} M}}" = 1.77 * 86400s
"M = 1.8*10^{27}kg"
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