84.9k views
0 votes
The Earth is 1.5 × 1011 m from the Sun and takes a year to make one complete orbit. It rotates on its own axis once per day. It can be treated approximately as a uniform-density sphere of mass 6 × 1024 kg and radius 6.4 × 106 m (actually, its center has higher density than the rest of the planet, and the Earth bulges out a bit at the equator). Using this crude approximation, calculate the following: (a) What is vCM ? (b) What is Ktrans ? (c) What is ω, the angular speed of rotation around its own axis? (d) What is Krot? (e) What is Ktot?

1 Answer

1 vote

Answer:

Part a)


v_(cm) = 2.98 * 10^4 m/s

Part b)


K_(trans) = 2.68 * 10^(33) J

Part c)


\omega = 7.27 * 10^(-5) rad/s

Part d)


KE_(rot) = 2.6 * 10^(29) J

Part e)


KE_(tot) = 2.68 * 10^(33) J

Step-by-step explanation:

Time period of Earth about Sun is 1 Year

so it is


T = 1 year = 3.15 * 10^7 s

now we know that angular speed of the Earth about Sun is given as


\omega = (2\pi)/(T)


\omega = (2\pi)/(3.15 * 10^7)

now speed of center of Earth is given as


v_(cm) = r\omega


r = 1.5 * 10^(11) m


v_(cm) = (1.5 * 10^(11))((2\pi)/(3.15 * 10^7))


v_(cm) = 2.98 * 10^4 m/s

Part b)

now transnational kinetic energy of center of Earth is given as


K_(trans) = (1)/(2)mv^2


K_(trans) = (1)/(2)(6 * 10^(24))(2.98 * 10^4)^2


K_(trans) = 2.68 * 10^(33) J

Part c)

Angular speed of Earth about its own axis is given as


\omega = (2\pi)/(T)


\omega = (2\pi)/(24 * 3600)


\omega = 7.27 * 10^(-5) rad/s

Part d)

Now moment of inertia of Earth about its own axis


I = (2)/(5)mR^2


I = (2)/(5)(6 * 10^(24))(6.4 * 10^6)^2


I = 9.83 * 10^(37) kg m^2

now rotational energy is given as


KE_(rot) = (1)/(2)I\omega^2


KE_(rot) = (1)/(2)(9.83 * 10^(37))(7.27 * 10^(-5))^2


KE_(rot) = 2.6 * 10^(29) J

Part e)

Now total kinetic energy is given as


KE_(tot) = KE_(trans) + KE_(rot)


KE_(tot) = 2.68 * 10^(33) + 2.6 * 10^(29)


KE_(tot) = 2.68 * 10^(33) J

User Aiden
by
4.4k points