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Ch 13: Newton's Theory of Gravity
Knight Calc - Physics for Scientists and Engineers 5th Edition
Knight Calc5th EditionPhysics for Scientists and EngineersISBN: 9780137344796당신이 사용하는 게 아니라요?교과서 변경
13장, 문제 68a

A satellite in a circular orbit of radius r has period T. A satellite in a nearby orbit with radius r + Δr, where Δr ≪ r, has the very slightly different period T + ΔT. Show that ΔT/T = (3/2) (Δr/r)

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Start by recalling Kepler's Third Law, which states that the square of the orbital period (T) of a satellite is proportional to the cube of the radius (r) of its orbit. Mathematically, this is expressed as: T^2 \(\propto\) r^3 or equivalently T^2 = k r^3, where k is a constant of proportionality.
Differentiate both sides of the equation T^2 = k r^3 with respect to r to find the relationship between changes in T and r. Using the chain rule, we get: 2T \(\frac{dT}{dr}\) = 3k r^2.
Rearrange the differentiated equation to isolate \(\frac{dT}{T}\): \(\frac{dT}{T}\) = \(\frac{3}{2}\) \(\frac{dr}{r}\). Here, \(\frac{dT}{T}\) represents the fractional change in the period, and \(\frac{dr}{r}\) represents the fractional change in the radius.
Recognize that for small changes in the radius and period, \(\Delta\) r and \(\Delta\) T can be used in place of dr and dT, respectively. Thus, the equation becomes: \(\frac{\Delta T}{T}\) = \(\frac{3}{2}\) \(\frac{\Delta r}{r}\).
Conclude that the fractional change in the orbital period is proportional to the fractional change in the orbital radius, with a proportionality constant of \(\frac{3}{2}\). This completes the derivation: \(\frac{\Delta T}{T}\) = \(\frac{3}{2}\) \(\frac{\Delta r}{r}\).

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주요 개념

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Kepler's Third Law

Kepler's Third Law states that the square of the orbital period of a planet is directly proportional to the cube of the semi-major axis of its orbit. For circular orbits, this can be expressed as T² ∝ r³, which implies that as the radius increases, the period increases, but at a specific rate determined by the gravitational force acting on the satellite.
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Kepler's Third Law

Differential Calculus

Differential calculus is a branch of mathematics that deals with the rates at which quantities change. In this context, it helps us understand how small changes in the radius (Δr) affect the orbital period (ΔT) of the satellite. By applying calculus, we can derive relationships between these small changes and express them in terms of ratios.
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Orbital mechanics is the study of the motion of objects in space under the influence of gravitational forces. It encompasses the principles governing satellite motion, including the relationship between radius, velocity, and period. Understanding these principles is crucial for analyzing how changes in orbital radius affect the period of a satellite's orbit.
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