Kepler’s Laws Planetary & Satellite Motion Pg 248-251 HRW History – Johannes Kepler Born in Germany in 1571 Assistant to Tycho Brahe (Danish) • Note: Newton was born in 1642 • Brahe, as an astronomer, meticulously • gathered planetary data Kepler analyzed Brahe’s Mars data and postulated 3 foundation laws of planetary motion (1609+) Kepler’s First Law - Ellipses Planets move in elliptical orbits with the Sun as one of the foci What are the implications for conservation of energy? Conservation of Energy – satellite motion Circular • PE, KE do not change Elliptical • PE max @ apogee • Max orbit radius • KE max @ perigee • Max speed Kepler’s Second Law – Equal Areas A line from the Sun to a planet sweeps out equal areas in equal times. “Conservation of Angular Momentum” v1r1 = v2r2 Kepler’s Third Law – Periods For all planets, the square of the orbital period (T) of a planet is proportional to the cube of the average orbital radius (do), or T2 do3, or T2/ do3 = constant = 42/GM, where • G = 6.67 x 10-11 N-m2/kg2 • M = mass of the foci body (ex. Sun) 4 3 2 T do GM 2 Practice Kepler’s 3rd Law What is the orbital period (T) of Neptune, in seconds and years, if its average orbital radius (do) is 4.495e12 and the mass of the sun is 1.99e30 kg? Solve T2 = 4π2/(GM) x do3 • T2 = 4π2/(6.67e-11*1.99e30)*(4.495e12)3 • T2 = 2.70e19 • T = 5.2e9 seconds • T = ~165 (Earth) years Example of Kepler’s 3rd Law Calculate K’s 3rd law constant for Neptune, given an orbital period (T) of 5.21e9 sec and an average orbital radius (do) of 4.495e12 m. Solve: T2/do3 • (5.21e9)2/(4.495e12)3 • = 2.97e-19 sec2/m3 Kepler Practice The shuttle orbits the Earth at 400 kms above the surface. If the radius and mass of the Earth are 6.37 x 106 m and 5.98 x 1024 kg, respectively: • What is the period of the shuttle’s orbit (in seconds)? Solve using K’s 3rd Law T2= 4π2do3/(GM) • T = 5541 sec • T = 92.3 minutes Kepler Practice Given that the moon’s period about the earth is 27.32 days and that the earthmoon distance is 3.84 x 108 m, • Calculate the mass of the earth. Solve using K’s 3rd Law: T2= 4π2do3/(GM) • M = 4π2do3/(GT2) • M = 6.01 x 1024 kg
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