Preparation problems


6-24. Suppose the moon were held in orbit not by gravity but by the tension in a massless cable. Estimate the magnitude of the tension in the cable.


Solution:

Were the moon held in orbit by a massless cable, the tension in the wire would be sufficient to provide the force necessary to keep the moon in a circular orbit. In other words,

Fnet = T = mmoon ar
So to find the tension in the cable, we need to know the radial acceleration of the moon. This we find using our uniform circular motion equation from our constants and equation sheet:
ar = v2
r
Recalling that r is the distance between the Earth and the moon, we can look up the values for mmoon, r and v from Appendix E:
mmoon
=
7.35 ×1022  kg
r
=
3.85 ×108  m
v
=
1000  m/s

Putting this all together, we get

T
=
mmoon ar
=
mmoon é
ê
ë
v2
r
ù
ú
û
=
mmoon v2
r
=
(7.35 ×1022  kg) (1000  m/s)2
3.85 ×108  m
T
=
1.91 ×1020  N


6-26. A mass m1 undergoes circular motion of radius R on a horizontal frictionless table, connected by a massless string through a hole in the table to a second mass m2 (see Figure 6-59 on page 146). If m2 is stationary, find (a) the tension in the string and (b) the period of the circular motion.


Solution:

The circular motion of the first mass is the result of the force being applied to the mass by the string. We can find the tension in the string by looking at a free-body diagram for the objects.

(a) Since we know the second mass is not moving, and hence not accelerating, we know the sum of the forces acting on it must be zero. This means we can quickly write down
Fnet
=
0
T - W2
=
0
T
=
W2
T
=
m2 g

(b) Now we need to find the period of rotation for the first mass. We can see that the forces in the y-direction balance, as the mass is remaining on top of the table. Thus the net force in the x-direction must be responsible for the circular motion. This means

Fnet = T = m1 ar
Since we know that the radial acceleration is given by
ar
=
v2
r
=
é
ê
ë
2 pr
t
ù
ú
û
2

 

r
ar
=
4 p2 r
t2
,
where t is the period of rotation, we can substitute into our equation above to get
T
=
m1 é
ê
ë
4 p2 r
t2
ù
ú
û
t2
=
m1 4 p2 r
T
t2
=
4 p2 m1 r
m2 g
t
=
  æ
Ö

4 p2 m1 r
m2 g
 
and we are done.


6-69. A space station is in the shape of a hollow ring with an outer diameter of 150 m. How fast should it rotate to simulate Earth's surface gravity-that is, so that the force exerted on an object by the outside wall is equal to the object's weight on Earth's surface?


Solution:

We want a situation in which the normal force exerted by the wall is equal to the mass of an object times its radial acceleration, or

N = m ar
But on the surface of the earth, this normal force would be equal to the object's weight, or
N = m g
So we quickly see that wee need the station to rotate such that
ar = g
Since we know that ar = v2/r, we see that
g
=
v2
r
=
é
ê
ë
2 pr
T
ù
ú
û

r
g
=
4 p2 r
T2
Since we want to know how fast the station spins, we should solve for the period, T. This gives us
T2
=
4 p2 r
g
T
=
  æ
Ö

4 p2 r
g
 
T
=
  æ
Ö

4 p2 (75  m)
9.8  m/s2
 
T
=
17.4  s
The station rotates one time in 17.4 s, so its angular velocity is
w = 1
17.4 s
= 0.058  rev/s = 3.45  rev/min

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Solutions translated from TEX by TTH, version 1.57.