Consider a space telescope sketched in Figure 4a. Suppose the space telescope is constructed out of cylindrical metal tube of uniform density. The mass of the tube is MT with an inner diameter Di and outer diameter Do. A circular disc antenna with diameter Da and mass Ma is attached at one end. The axis of symmetry of the telescope and the rotational axis of the disc antenna are co-linear. The mass of the rest of the internal structures and communication electronics are negligibly small. Calculate the rotational inertia of the space telescope about its symmetric Z axis. 4a.
Consider a space telescope sketched in Figure 4a. Suppose the space telescope is constructed out of cylindrical metal tube of uniform density. The mass of the tube is MT with an inner diameter Di and outer diameter Do. A circular disc antenna with diameter Da and mass Ma is attached at one end. The axis of symmetry of the telescope and the rotational axis of the disc antenna are co-linear. The mass of the rest of the internal structures and communication electronics are negligibly small. Calculate the rotational inertia of the space telescope about its symmetric Z axis. 4a.
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
Transcribed Image Text:Consider a space telescope sketched in Figure 4a. Suppose the space
telescope is constructed out of cylindrical metal tube of uniform density. The
mass of the tube is MT with an inner diameter Dj and outer diameter Do. A
circular disc antenna with diameter Da and mass Ma is attached at one end.
4a.
The axis of symmetry of the telescope and the rotational axis of the disc
antenna are co-linear. The mass of the rest of the internal structures and
communication electronics are negligibly small. Calculate the rotational
inertia of the space telescope about its symmetric Z axis.
Suppose the telcacope is launched from the cargo bay of the space shuttle. The
space shuttle first adjust it orientation so that the axis of the telescope is
pointing at a distant star so that it can collect signal from the star. The
telescope is set into a spinning motion by two jets installed symmetrically on
the circumference of the telescope (See figure 4b) before it is released. The
torque generated by each jet is graphed in figure 4c. Both jets are fired
simultaneously. What is the purpose of setting the space telescope into
rotational motion? Calculate the final rotational velocity w of the space
telescope at the end of the rocket burnt.
What is the angular momentum L (magnitude and direction) of the telescope
about its rotational Z axis if the rotation is clockwise direction?
What will be the angular momentum L two days later after it was launch?
Explain.
4b.
4c.
4d.
Feg 4a
Tap viaw
Fig 4b
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