Ch. 12: Gravitation
Why is the Earth round?
Why do animals have bones?
Why do we live in a “solar system?”
Why is there a Moon?
(12.1) Newton’s Law of
Gravitation
•Note: 3rd Law tells us F
g(1 on 2) = - Fg(2 on 1)
→ →
1798: G found to be 6.673 x 10-11 N m2/kg2
F
g=
G m
1m
2r
2Find the magnitude and direction of the net
gravitational force exerted on the small star by the two large stars.
Note: A sphere can be treated as though all its mass is concentrated at its center
Inner Space
Down in a cave below the surface of the Earth there is
F
gfor Objects Near the Earth
M
Em
R
Er
(r > RE)
F
gfor Objects On the Earth’s Surface
(r = RE)F
g=
M
Em
R
EF
gfor Objects Inside the Earth
M
Em
R
E(r < RE)
*Using calculus, it can be shown that when r < RE
only the mass within r exerts a force!
r
M
But what is M?
F
gr
“linear”
“inverse square”
Where is Fg largest/smallest?
RE
Inner Space
Down in a cave below the surface of the Earth there is
Weight
•when an object is on the Earth, Fg from the rest of the universe may be ignored
F
g=
G
M
Em
R
E2•so the only gravitational force is:
mg
=
G M
Em
R
E2•we call this “weight” (a.k.a. mg), thus:
g
=
G M
ER
E2Example 12.3 Mission to Mars
RM = 3.4 x 106 m M
M = 6.42 x 1023 kg
wlander = 39,200 N
(12.3) Gravitational Potential
Energy
U
=
mgy
Where did this come from? F = − dU
dy = −mg Fg = −mg y
Guess:
U
= −
G m
1m
2r
Check:
−
dU
dr
= −
G m
1m
2r
2F
g=
−
G m
1m
2r
r
2
M
Em
R
Er
F
GFor objects at any distance from Earth:
U =
−
G M
Em
Notes:
1. U always < 0
2. As r increases, U increases (less negative)
3. As r decreases, U decreases (more negative)
U
r
This is a bound system (recall marble analogy)
RE
Problem 12.65
A hammer with mass
m
is dropped
from rest from a height
h
above the earth’s
surface. This height is not necessarily small
compared to the radius
R
Eof the earth. If
you ignore air resistance, derive an
expression for the speed
v
of the hammer
when it reaches the surface of the earth.
Your expression should involve
h
,
R
E, and
Example 12.5 Escape Speed
M
Em
R
Ev
escapeNote: To escape means to barely reach r= as
you come to rest!
U
r
RE
−G ME m RE
Example 12.5 Escape Speed
vescape = 2 G ME RE
vescape = 1.12 x 104 m/s 25,000 mi/h
Why launch from Cape Canaveral?
M
Em
R
Ev
escapem
•escape from Earth
is extreme!
(12.4) Motion of Satellites
•if launched at lower
speeds, an object
Video Quiz
1. How does gEarth compare to gMoon?
2. Why are astronauts “weightless” in their spacecraft?
3. What is a satellite?
4. How far away are our closest satellites? Our farthest?
5. What are the periods of these satellites, respectively?
(12.4) Motion of Satellites
•Let’s consider circular orbits, to which Newton’s
R
Er
v
Fg
G M
Em
r
2=
mv
2r
v = G ME r
•for a given radius r, the speed of circular orbit
is uniquely determined
•orbital speed is independent of satellite’s mass
•since v = 2r/T, we can find an expression for the period of a circular orbit
T = 2 r3/2
GME
•for orbits with larger r, speed is ______ and period is _______
Note:
slower longer
e.g. ISS Moon
r = 6800 km
T = 93 min v = 7.7 km/s
r = 384,000 km
T = 27 days v = 1 km/s
RE r
v
ME m
Notes:
1. for a given r, E is uniquely determined
3. as r increases, E increases (less negative)
4. As r decreases, E decreases (more negative)
Example 12.6
Suppose you want to place a 1000-kg weather satellite 300 km above the earth’s surface.
a) What speed and period must it have?
b) How much work must be done to place it in orbit?
c) How much additional work would have to be done to make this satellite escape the earth?
A space shuttle and a satellite are in the
same circular orbit, but on opposite sides
of the Earth. How can the
shuttle catch up to the
satellite?
(12.5) Kepler’s Laws of
Planetary Motion
1619: Kepler, building on earlier work of
Copernicus and Brahe, discovered three laws describing the motion of planets
(12.5) Kepler’s Laws of
Planetary Motion
1619: Kepler, building on earlier work of
Copernicus and Brahe, discovered three laws describing the motion of planets
2. A line from the sun to a planet
sweeps out equal areas in equal times.
This can be explained using conservation of angular momentum:
L = mvr
3. The periods of the planets are proportional to the 3/2 power of the semi-major axis of their
orbits.
T = 2
a
3/2GM
sFor a satellite in circular orbit around the Earth, a = r and MS ME