/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 9 Two satellites \(S_{1}\) and \(S... [FREE SOLUTION] | 91Ó°ÊÓ

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Two satellites \(S_{1}\) and \(S_{2}\) describe circular orbits of radii \(r\) and \(2 r\) respectively around a planet. If the orbital angular velocity of \(S_{1}\) is \(\omega\), the orbital angular velocity of \(S_{2}\) is (A) \(\frac{\omega}{2 \sqrt{2}}\) (B) \(\frac{\omega \sqrt{2}}{3}\) (C) \(\frac{\omega}{\sqrt{2}}\) (D) \(\omega \sqrt{2}\)

Short Answer

Expert verified
The orbital angular velocity of S2 is \(\frac{\omega}{2\sqrt{2}}\).

Step by step solution

01

Write down the formula for gravitational force

The gravitational force acting on the satellites is given by Newton's law of gravitation: \[F = G\frac{Mm}{r^2}\] where F is the gravitational force, G is the gravitational constant, M is the mass of the planet, m is the mass of the satellite, and r is the distance between the planet and the satellite.
02

Write down the formula for centripetal force

The centripetal force acting on a satellite in a circular orbit is given by the formula: \[F = m\omega^2r\] where F is the centripetal force, m is the mass of the satellite, ω is the angular velocity, and r is the radius of the orbit.
03

Set the gravitational force equal to the centripetal force for S1 and S2

For S1, we have: \[G\frac{Mm}{r^2} = m\omega^2r\] For S2, we have: \[G\frac{Mm}{(2r)^2} = m\omega_2^2(2r)\] where ω is the orbital angular velocity of S1, and ω_2 is the orbital angular velocity of S2.
04

Solve the equations for ω_2

Divide the equation for S2 by the equation for S1 to eliminate M and m: \[\frac{G\frac{Mm}{(2r)^2}}{G\frac{Mm}{r^2}} = \frac{\omega_2^2(2r)}{\omega^2r}\] Simplify the equation: \[\frac{1}{4} = \frac{2\omega_2^2r}{\omega^2r}\] Solve for ω_2: \[\omega_2^2 = \frac{\omega^2}{8}\] Take the square root of both sides: \[\omega_2 = \frac{\omega}{\sqrt{8}}\] Simplify: \[\omega_2 = \frac{\omega}{2\sqrt{2}}\] This corresponds to option (A). So, the orbital angular velocity of S2 is \(\frac{\omega}{2\sqrt{2}}\).

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