Preparation problems


9-12. At what altitude will a satellite complete a circular orbit of the Earth in 2.0 hours?


Solution:

We need to find a relationship between the period of a circular orbit and its altitude. We can start by considering the relationship between the gravitational force and the radial force keeping the satellite in uniform circular motion

Fg
=
m ar
GMm
r2
=
m v2
r
v2
=
GM
r
However, we also know that the velocity of an object in uniform circular motion is given by
v = 2 pr
T
Substituting this in, we get
v2
=
GM
r
æ
ç
è
2 pr
T
ö
÷
ø
2

 
=
GM
r
r3
=
GM
4 p2
T2
r
=
é
ê
ë
GM
4 p2
T2 ù
ú
û
(1/3)

 
This will give us the radius of the orbit. If we recall that the altitude of the orbit is the height above the Earth's surface, we see that we want to know
h = r - RE = é
ê
ë
GM
4 p2
T2 ù
ú
û
(1/3)

 
- RE
where RE is the radius of the Earth. Plugging in our known values, we get an answer of
h = 1690  km


9-21. Where should a satellite be placed to orbit the Sun with a period of 100 days?


Solution:

We need to find a relationship between the radius of a circular orbit and its period. We can start by considering the relationship between the gravitational force and the radial force keeping the satellite in uniform circular motion

Fg
=
m ar
GMm
r2
=
m v2
r
v2
=
GM
r
where M is the mass of the sun and r is the distance at which the satellite orbits. However, we also know that the velocity of an object in uniform circular motion is given by
v = 2 pr
T
Substituting this in, we get
v2
=
GM
r
æ
ç
è
2 pr
T
ö
÷
ø
2

 
=
GM
r
r3
=
GM
4 p2
T2
r
=
é
ê
ë
GM
4 p2
T2 ù
ú
û
(1/3)

 
Recalling that T = 8.64 ×106 s, we get an answer of
r = 6.31 ×1010  m


9-22. Determine the orbital period of the Hubble Space Telescope, which orbits Earth at an altitude of 610 km.


Solution:

We need to find a relationship between the altitude of a circular orbit and its period. We can start by considering the relationship between the gravitational force and the radial force keeping the satellite in uniform circular motion

Fg
=
m ar
GMm
r2
=
m v2
r
v2
=
GM
r
where M is the mass of the sun and r is the distance at which the satellite orbits. Additionally, we also know that the velocity of an object in uniform circular motion is given by
v = 2 pr
T
Substituting this in, we get
v2
=
GM
r
æ
ç
è
2 pr
T
ö
÷
ø
2

 
=
GM
r
T2
=
4 p2
GM
r3
T
=
  æ
Ö

4 p2
GM
(RE + h)3
 
For the last step, we have used the fact that we can write the radius as r = RE + h, where RE is the radius of the Earth and h is the altitude of the orbit. Putting in our known numbers, we get
T = 5806  s = 1  hour  37  minutes



Follow-up problems


9-9. A sensitive gravitometer is carried to the top of Chicago's Sears Tower, where its reading for the acceleration of gravity is 0.00136 m/s2 lower than at street level. Find the height of the building.


Solution:

We start by writing an equation to represent the information we are given in the problem:

Dg = gtop - gbottom = -0.00136 m/s2
(1)
Now we can find the acceleration due to gravity at any distance from the center of the earth by recalling
Fg
=
m g
=
GMm
r2
g
=
GM
r2
Knowing this, we can rewrite Eq. (1) as
Dg
=
gtop - gbottom
=
GM
(RE+h)2
- GM
RE2
Here we have assumed that the bottom of the Sears Tower is at a distance RE (mean radius of Earth) from the center of Earth. While this is not exactly true, it will be close enough for our problem. Now we simply must solve for h, the height of the building. Doing this we get
Dg
=
GM
(RE+h)2
- GM
RE2
GM
(RE+h)2
=
Dg + GM
RE2
1
(RE+h)2
=
Dg
GM
+ 1
RE2
(RE+h)2
=
1
Dg
GM
+ 1
RE2
h
=
  æ
Ö

1
Dg
GM
+ 1
RE2
 
- RE
Plugging in our known values, we get an answer of
h = 441  m

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Solutions translated from TEX by TTH, version 1.57.