A spherical asteroid with radius\(r = 123\;{\rm{m}}\)and mass\(M = 2.25 \times {10^{10}}\;{\rm{kg}}\)rotates about an axis at four revolutions per day. A “tug” spaceship attaches itself to the asteroid’s south pole (as defined by the axis of rotation) and fires its engine, applying a force F tangentially to the asteroid’s surface as shown in Fig. 8–65. If\(F = 285\;{\rm{N}}\)how long will it take the tug to rotate the asteroid’s axis of rotation through an angle of 5.0° by this method?

Short Answer

Expert verified

The time taken by the tug to rotate the asteroid’s axis of rotation is 27 h.

Step by step solution

01

Identification of the given data

The radius of the asteroid is\(r = 123\;{\rm{m}}\).

The mass of the asteroid is\(m = 2.25 \times {10^{10}}\;{\rm{kg}}\).

The magnitude of force applied to the asteroid is\(F = 285\;{\rm{N}}\).

The angle of rotation is \(\theta = \frac{5}{{360}} \times 2\pi \;{\rm{rad}} = \frac{\pi }{{36}}\;{\rm{rad}}\).

The angular speed of the asteroid is \(\omega = \frac{{8\pi \;{\rm{rad}}}}{{86400\;{\rm{s}}}} = \frac{{8\pi }}{{86400}}\;{\rm{rad/s}}\).

02

Definition of angular momentum

Angular momentum is the rotational equivalent of the linear momentum of a body. It is expressed as the product of the moment of inertia and angular velocity.

\(L = I\omega \) … (i)

03

Newton’s second law for rotational dynamics

The rotational analog of Newton’s second law of motion states that the net torque acting on a body is equal to the time rate of change of angular momentum. It is given as:

\(\tau = \frac{{\Delta L}}{{\Delta t}}\)

04

Calculation of the time taken by the tug to rotate the asteroid’s axis of rotation

The spaceship applies a torque on the asteroid which changes the direction of its angular momentum. Also, torque can be written as the time rate of change of angular momentum.

\(\begin{aligned}{c}\tau = \frac{{\Delta L}}{{\Delta t}}\\ = \frac{{L\Delta \theta }}{{\Delta t}}\\\Delta t = \frac{{L\Delta \theta }}{\tau }\end{aligned}\) … (ii)

The moment of inertia of the asteroid (solid sphere) is\(I = \frac{2}{5}m{r^2}\).

Substitute equation (i) in (ii).

\(\begin{aligned}{c}\Delta t = \frac{{I\omega \Delta \theta }}{\tau }\\ = \frac{{I\omega \Delta \theta }}{{rF}}\\ = \frac{{\left( {\frac{2}{5}m{r^2}} \right)\omega \Delta \theta }}{{rF}}\\ = \frac{{\frac{2}{5}mr\omega \Delta \theta }}{F}\end{aligned}\) … (iii)

Substituting the known numerical values in equation (iii), you get:

\(\begin{aligned}{c}\Delta t = \frac{{\frac{2}{5}\left( {2.25 \times {{10}^{10}}\;{\rm{kg}}} \right)\left( {123\;{\rm{m}}} \right)\left( {\frac{{8\pi }}{{86400}}\;{\rm{rad/s}}} \right)\left( {\frac{\pi }{{36}}\;{\rm{rad}}} \right)}}{{285\;{\rm{N}}}}\\ = 9.860 \times {10^4}\;{\rm{s}}\\ = 9.860 \times {10^4}\;{\rm{s}} \times \frac{{1\;{\rm{hr}}}}{{3600\;{\rm{s}}}}\\ \approx 27\;{\rm{h}}\end{aligned}\)

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