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Physics 201: Lecture 24, Pg 1
Chapter 13
The beautiful rings of Saturn consist of countless centimeter-sized ice
crystals, all orbiting the planet under the influence of gravity.
Goal: To use Newton’s theory of gravity to understand the motion of satellites and planets.
Physics 201: Lecture 24, Pg 2
Who discovered the basic laws of planetary orbits?
A. NewtonB. KeplerC. FaradayD. EinsteinE. Copernicus
Physics 201: Lecture 24, Pg 3
What is geometric shape of a planetary or satellite orbit?
A. CircleB. HyperbolaC. SphereD. ParabolaE. Ellipse
Physics 201: Lecture 24, Pg 4
The value of g at the height of the space shuttle’s orbit is
A. 9.8 m/s2.
B. slightly less than 9.8 m/s2.
C. much less than 9.8 m/s2.
D. exactly zero.
Physics 201: Lecture 24, Pg 5
Newton proposed that every object in the universe attracts every other object.The Law: Any pair of objects in the Universe attract each other with a force that is proportional to the products of their masses and inversely proportional to the square of their distance
Newton’s Universal “Law” of Gravity
Physics 201: Lecture 24, Pg 6
Newton’s Universal “Law” of Gravity
2by1on12221
1by 2on r̂ Fr
mmGF
“Big” G is the Universal Gravitational Constant
G = 6.673 x 10-11 Nm2 / kg2
Two 1 Kg particles, 1 meter away Fg= 6.67 x 10-11 N(About 39 orders of magnitude weaker than the electromagnetic force.)
The force points along the line connecting the two objects.
Physics 201: Lecture 24, Pg 7
Newton’s Universal “Law” of Gravity
2by1on12221
1by 2on r̂ Fr
mmGF
You have three 1 kg masses, 1 at the origin, 2 at (1m, 0) and 3 at (0, 1m). What would be the Net gravitational force on object 1 by objects 2 & 3?
G = 6.673 x 10-11 Nm2 / kg2
Two 1 Kg particles, 1 meter away Fg= 6.67 x 10-11 N
Each single force points along the line connecting two objects.
3by1on13221
1by 3on r̂ Fr
mmGF
Fg=9.4 x 10-11 N along diagonal
Physics 201: Lecture 24, Pg 8
Motion Under Gravitational Force
Equation of Motion
r̂)(r
22
2
r
MmG
dttd
m
If M >> m then there are two classic solutions that depend on the initial r and v
Elliptical and hyperbolic paths
Physics 201: Lecture 24, Pg 9
Anatomy of an ellipse
a: Semimajor axis b: Semiminor axis c: Semi-focal length a2 =b2+c2
Eccentricity e = c/a
If e = 0, then a circle
Most planetary
orbits are close to
circular.
12
2
2
2
b
y
a
x
Physics 201: Lecture 24, Pg 10
A little history Kepler’s laws, as we call them today, state that
1. Planets move in elliptical orbits, with the sun at one focus of the ellipse.
2. A line drawn between the sun and a planet sweeps out equal areas during equal intervals of time.
3. The square of a planet’s orbital period is proportional to the cube of the semimajor-axis length.
Focus Focus
Physics 201: Lecture 24, Pg 11
Kepler’s 2nd Law The radius vector from the sun to a planet sweeps out equal
areas in equal time intervals (consequence of angular momentum conservation).
Why?
r̂
)(r
2
2
2
r
MmG
dt
tdm
Physics 201: Lecture 24, Pg 12
Conservation of angular momentum Area of a parallelogram = base x height
A
C
||21 rdrdA
sin|| ACCA
dtvrddtvrdA ||2
1
mdtvmr
dA|)(|2
1
||||21 Lpr
dt
dAm
L is constant (no torque)
Physics 201: Lecture 24, Pg 13
Kepler’s 3rd Law
Square of the orbital period of any planet is proportional to the cube of semimajor axis a.
3
Sun
22 4
aGM
T
222
)2
(T
rrrv
ac
2Sun
lCentripeta r
mMGmaF c
2Sun2)
2(
rM
GT
r
23 Tr
Physics 201: Lecture 24, Pg 14
Suppose an object of mass m is on the surface of a planet of mass M and radius R. The local gravitational force may be written as
Little g and Big G
where we have used a local constant acceleration:
On Earth, near sea level, it can be shown that gsurface ≈ 9.8 m/s2.
surfacemgFG
2surface RGM
g
mMMm R
mGMF ,2by on r̂
Physics 201: Lecture 24, Pg 15
Cavendish’s Experiment
F = m1 g = G m1 m1 / r2
g = G m2 / r2
If we know big G, little g and r then will can find the mass of the Earth!!!
Physics 201: Lecture 24, Pg 16
Orbiting satellites vt = (gr)½
Net Force: ma = mg = mvt
2 / r gr = vt
2
vt = (gr)½
The only difference is that g is less because you are further from the Earth’s center!
Physics 201: Lecture 24, Pg 17
Geostationary orbit
Physics 201: Lecture 24, Pg 18
Geostationary orbit
The radius of the Earth is ~6000 km but at 36000 km you are ~42000 km from the center of the earth.
Fgravity is proportional to 1/r2 and so little g is now ~10 m/s2 / 50 vT = (0.20 * 42000000)½ m/s = 3000 m/s
At 3000 m/s, period T = 2 r / vT = 2 42000000 / 3000 sec =
= 90000 sec = 90000 s/ 3600 s/hr = 24 hrs
Orbit affected by the moon and also the Earth’s mass is inhomogeneous (not perfectly geostationary)
Great for communication satellites
(1st pointed out by Arthur C. Clarke)
Physics 201: Lecture 24, Pg 19
Tuesday
All of Chapter 13