Q.Explain Kepler's laws of planetary motion and deduce Newton's law of gravitation from them.
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Start your 14-day free trial to unlock the full solution →Kepler's three laws (elliptical orbits, equal areas in equal times, T^2 proportional to a^3) combine with the centripetal-force requirement to give Newton's inverse-square law of gravitation, F = GMm/r^2.
Kepler's Laws of Planetary Motion:
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Law of Orbits: Every planet moves around the Sun in an elliptical orbit, with the Sun located at one of the two foci of the ellipse.
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Law of Areas: The line joining a planet to the Sun (the radius vector) sweeps out equal areas in equal intervals of time. This means a planet moves faster when closer to the Sun (perihelion) and slower when farther away (aphelion) -- a direct consequence of the conservation of angular momentum, since gravity is a central force.
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Law of Periods: The square of the time period (T) of revolution of a planet around the Sun is directly proportional to the cube of the semi-major axis (a) of its elliptical orbit:
T^2 proportional to a^3, i.e. T^2 = k*a^3 (k a constant, same for all planets orbiting the Sun).
Deducing Newton's Law of Gravitation (approximating planetary orbits as circular, radius r):
For a planet of mass m moving in a circular orbit of radius r with speed v around the Sun, the centripetal force needed to keep it in orbit must be supplied by the Sun's gravitational pull F:
F = m v^2 / r = m omega^2 r, where omega = 2*pi/T
So: F = m * (2pi/T)^2 * r = 4pi^2mr / T^2
From Kepler's third law, T^2 = k * r^3 (using a = r for a circular orbit). Substituting:
F = 4pi^2mr / (kr^3) = (4*pi^2/k) * (m/r^2)
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