Universal Gravitation
Universal Gravitation
Universal Gravitation
IB 12
Law 1: All planets orbit the Sun in elliptical paths with the
Sun at one focus.
Formula
T 2 r 3
T 2 kr 3
T r
3
2
2. The force between two spherical masses whose separation is large compared to their radii is the same as if
the two spheres were point masses with their masses concentrated at the centers of the spheres.
Sun
Earth
Point mass
Formula
IB 12
m1 m2
r2
G m1 m2
Fg =
r2
Fg
Gravitational Constant :
G = 6.77 x 10-11 N m2/kg2
Derivation
Fc mac
GMm mv 2
r2
r
GM
v2
r
2 r
but v
T
GM 2 r
r
T
GM 4 2 r 2
r
T2
T 2 4 2
r 3 GM
T 2 4 2
r 3 GM
1 year 365.25days 24hours 3600s
4 2
3
6.67 x1011 M s
1.50 x1011 m
2
M S 2.0 x1030 kg
accepted value=1.99 x1030 kg
2
What is the resultant gravitational force on the Earth from the Sun and Moon, as shown below?
Average Earth-Sun distance = 1.50 x 1011 m
Sun
Earth
Moon
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Symbol: g
Point mass
Formula: g = Fg / m
g = Fg /m
g = (GMm/r2)/m
g = GM/r2
Type: vector
g = GM/r2
go = G Mp / Rp2
go = G
ME/Re2
go
g ratio
g/go = RE2/r2
IB 12
Earth
Moon
3. a) What is the resultant gravitational field strength at a point midway between the Earth and Moon?
b) What is the resultant gravitational force acting on a 1500. kg space probe at this location?
Earth
Moon
4. a) Is there a point where the resultant gravitational field strength of the Earth and Moon is zero? If so, where?
b) What is the resultant gravitational force acting on a 1500. kg space probe at this location?
IB 12
Difference in gravitational potential energy between any two points in a gravitational field:
EP = mgh
EP = -400 J
EP = -100 J
EP = 0
Formula:
IB 12
Ep = - GMm/r
EP = -Gm1m2/r
Formula not valid
inside planet
Ep at surface
Ep = -GMpm/Rp
Symbol: V
Units: J
Type: scalar
What is the gravitational potential energy of a 5000 kg satellite:
a) on the surface of the Earth?
Gravitational Potential
Gravitational potential at a
point in a gravitational field:
work done per unit mass to bring a small point mass in from infinity to
that point in the gravitational field
Formulas:
Gravitational Potential
vs. distance
Difference in
gravitational potential:
V = W/m
V = Ep/m
Gravitational
potential at a point:
Symbol: V
V = Ep/m
V = -GM/r
Units: J/kg
Type: scalar
V at surface
Vo = -GMp/Rp
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IB 12
c) What is the change in potential in moving from the surface to this new location?
d) What is the minimum amount of energy needed to lift a 5000 kg satellite to this location?
2. What is the net gravitational potential at a spot midway between the Earth and the Sun?
Sun
Earth
3. Derive an expression for the gravitational potential at the surface of a planet in terms of the gravitational field strength.
Escape Speed
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Escape Speed: minimum initial speed an object must have at the surface of a planet in order to escape the
gravitational attraction of the planet
Travel to infinity
Just make it means velocity is zero at infinity means EK is zero at infinity as well as EP
Eo = Ep + Ek
Ef = Ep
Planet
Satellite Motion
Natural Satellites
Period of a satellite:
T r
2
Artificial Satellites
Acceleration of a satellite:
Weightlessness
v = 2 r/T
ac = 42 r/T2
3
2
ac = g = GM/r2
Free fall
Fc mac
ac = v2/r
v = 2 r/T
T 2 kr 3
T r
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Orbital motion
GMm mv 2
r2
r
GM
v2
r
GM
v
r
Deep space
IB 12
Kinetic Energy
Energy Derivations
Total Energy
Kinetic Energy
Total Energy
RE
Comparisons:
A 1500 kg satellite is to be put into orbit around the Earth at an altitude of 200 km.
a) How much potential energy will the satellite
have at this altitude?
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Comparisons
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IB 12
On the diagram at right:
a) Sketch the gravitational field around the point mass.
gravitational potential gradient: the gravitational field is the negative gradient of the gravitational
potential with respect to distance
Formula
-70 J/kg
-80 J/kg
B
derive g = -V/r
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Practice Questions
1. a) Calculate the gravitational force the Sun exerts
on the Earth.
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4. a) Calculate the resultant gravitational field at a spot
midway between the Earth and Sun.
Mars
b) How much gravitational potential energy does the satellite have on the surface of Mars?
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Universal
Fg m1 m2
Gravitationa
1
l Constant
Fg 2
r
(G):
G = 6.77 x
6. A 5000. kg satellite is placed in a low altitude orbit.
10-11 N
2
2
m /kg
a) If the altitude is sufficiently low, what is the approximate radius of the satellites orbit?
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g) What is the minimum amount of energy needed to lift the satellite into this orbit?
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