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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: 9780137344796Non è quello che usi tu?Cambia libro di testo
Capitolo 13, Problema 54b

In 2014, the European Space Agency placed a satellite in orbit around comet 67P/Churyumov-Gerasimenko and then landed a probe on the surface. The actual orbit was elliptical, but we’ll approximate it as a 50-km-diameter circular orbit with a period of 11 days. What is the mass of the comet?

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Step 1: Start by identifying the relevant formula for orbital motion. The gravitational force provides the centripetal force for the satellite's circular orbit. Use the formula for orbital period: \( T = 2\pi \sqrt{\frac{r^3}{G M}} \), where \( T \) is the orbital period, \( r \) is the orbital radius, \( G \) is the gravitational constant, and \( M \) is the mass of the comet.
Step 2: Rearrange the formula to solve for the mass of the comet \( M \): \( M = \frac{4\pi^2 r^3}{G T^2} \). This equation relates the mass of the comet to the orbital radius and period of the satellite.
Step 3: Convert the given values into SI units. The orbital radius \( r \) is half the diameter, so \( r = \frac{50\,\text{km}}{2} = 25\,\text{km} = 25,000\,\text{m} \). The orbital period \( T \) is 11 days, so convert it to seconds: \( T = 11 \times 24 \times 60 \times 60 \,\text{s} \).
Step 4: Substitute the known values into the formula. Use \( G = 6.674 \times 10^{-11} \, \text{m}^3 \text{kg}^{-1} \text{s}^{-2} \), \( r = 25,000 \, \text{m} \), and \( T \) in seconds. The equation becomes \( M = \frac{4\pi^2 (25,000)^3}{(6.674 \times 10^{-11})(T^2)} \).
Step 5: Simplify the expression to calculate \( M \). Perform the operations step by step: cube the radius \( r^3 \), square the period \( T^2 \), and then compute the numerator and denominator to find the mass of the comet. Ensure all units are consistent throughout the calculation.

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Gravitational Force

Gravitational force is the attractive force between two masses, described by Newton's law of universal gravitation. It states that the force is proportional to the product of the masses and inversely proportional to the square of the distance between their centers. This concept is crucial for understanding how celestial bodies interact and maintain their orbits.
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Orbital Mechanics

Orbital mechanics is the study of the motion of objects in space under the influence of gravitational forces. It involves understanding how the shape, size, and period of an orbit relate to the mass of the central body. In this context, the period of the satellite's orbit can be used to derive the mass of the comet using Kepler's laws.
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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 simplified to relate the period and radius to the mass of the central body. This law is essential for calculating the mass of the comet based on the satellite's orbital characteristics.
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