Transcript g = GM R 2

Gravitation
Gravitational Force and Field
Newton proposed that a force of attraction
exists between any two masses.
This force law applies to point masses not
extended masses
However the interaction between two
spherical masses is the same as if the masses
were concentrated at the centres of the
spheres.
Newton´s Law of Universal
Gravitation
Newton proposed that
“every particle of matter in the universe
attracts every other particle with a force
which is directly proportional to the product
of their masses, and inversely proportional
to the square of their distance apart”
This can be written as
F = G m1m2
r2
Where G is Newton´s constant of
Universal Gravitation
It has a value of 6.67 x 10-11 Nm2kg-2
Gravitational Field Strength
A mass M creates a gravitational field in
space around it.
If a mass m is placed at some point in
space around the mass M it will
experience the existance of the field in
the form of a gravitational force
We define the graviational field strength
as the ratio of the force the mass m
would experience to the mass, m
That is the graviational field strength at
a point, is the force exerted per unit
mass on a particle of small mass placed
at that point
The force experienced by a mass m placed a
distance r from a mass M is
F = G Mm
r2
And so the gravitational field strength of the
mass M is given by dividing both sides by m
g=GM
r2
Field Strength at the
Surface of a Planet
If we replace the particle M with a
sphere of mass M and radius R then
relying on the fact that the sphere
behaves as a point mass situated at its
centre the field strength at the surface
of the sphere will be given by
g= GM
R2
If the sphere is the Earth then we have
g = G Me
Re2
But the field strength is equal to the
acceleration that is produced on the mass,
hence we have that the acceleration of free
fall at the surface of the Earth, g
g = G Me
Re2
Gravitational Potential Energy
We have been using U g  mgh
To calculate the change in gravitational
energy for objects close to the surface
of the earth.
This doesn’t work if we are talking about
objects that are not close to the
surface.
Gravitational Potential Energy
Now we have to develop a new formula
r2
U g  Wgrav   Fdr
r1
r2
GmE m
F 
2
r
GmE m
GmE m GmE m
U g   
dr 

2
r
r2
r1
r1
GmE m
U g  
r
Gravitational Potential Energy Curve
Escape Speed
An object can escape earth’s orbit
when:
K  Ug
So:
GmE m
1
mv

2
R
2
2GM
v
R
Motion of Satellites
An object shot
horizontally will
follow a parabolic
path
If it is moving fast
enough then the
curvature of the
earth matters.
If you get the
perfect speed it
will just fall in a
circle around the
earth.
Motion of Satellites
In order for a satellite to orbit the earth in a
circular orbit, the force of gravity must be
equal to the force necessary for circular
motion at that orbital radius.
GmE m
Fg 
R2
mv
Fc 
R
2
Set them equal and solve for speed
GmE
v
R
Notice that the speed does not depend on the
mass of the satellite, but the speed does depend
on the radius of the orbit.
Period of Rotation for a
Circular Orbit
Period is the time taken for the satellite
to make one complete orbit.
GmE
v
R
2R
Gm

T
R
2R
v
T
2R
T
GmE
3/ 2
Kepler’s Laws of Planetary
Motion
Each planet moves in an elliptical orbit,
with the sun at one focus of the ellipse.
A line from the sun to a given planet
sweeps out equal areas in equal times.
The period of the planets are
proportional to the 3/2 power of the
major axis lengths of their orbits.
1st Law: Elliptical Orbits
Actual orbits of planets in our solar system mostly
circular
We approximate them as circular to save time.
2nd Law: Equal Areas in Equal Times
Derives from
constant angular
momentum.
Also keeps total
energy constant.

Greatest Kinetic
Energy when
Gravitational
Energy is the
most negative.
3rd Law: Period of Elliptical Orbit
We derived this relationship for circular
orbits.
You could do the same for elliptical
orbits.
2a
T
Gm
3/ 2
a is the length of the semi-major axis