Gravity and Kepler's Laws: Understanding Planetary Motion, Study notes of Physics

The fundamental concepts of gravity and kepler's laws, which describe the motion of planets around the sun. Topics include elliptical orbits, equal areas swept out in equal times, and the relationship between a planet's period and its semimajor axis. The document also covers newton's law of gravity, the distinction between gravitational and inertial mass, and the derivation of kepler's laws.

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Pre 2010

Uploaded on 08/30/2009

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Gravity (Chapter 11)
Kepler’s Laws
Example of a successful phenomenology at the cradle of science (astronomical
observations by Brahe).
1. All planets move on elliptical orbits with the sun at one focus. (Ellipse: see
mathworld.)
2. A line joining any planet to the sun sweeps out equal areas in equal times (figure
11-4 of Tipler-Mosca).
3. The square of the period of any planet is proportional to the cube of the
semimajor axes of its orbit
T2=C r2.
Astronomical unit (AU): The mean earth-sun distance
1 AU = 1.50 ×1011 m = 93.0×106mi .
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Gravity (Chapter 11)

Kepler’s Laws

Example of a successful phenomenology at the cradle of science (astronomical observations by Brahe).

  1. All planets move on elliptical orbits with the sun at one focus. (Ellipse: see mathworld.)
  2. A line joining any planet to the sun sweeps out equal areas in equal times (figure 11-4 of Tipler-Mosca).
  3. The square of the period of any planet is proportional to the cube of the semimajor axes of its orbit T 2 = C r^2.

Astronomical unit (AU): The mean earth-sun distance

1 AU = 1. 50 × 1011 m = 93. 0 × 106 mi.

Newton’s Law of Gravity

Force of attraction between each pair of point particles (figure 11-6 of Tipler-Mosca)

F^ ~ 12 = −G m^1 m^2 r^212

ˆr 12 = −

G m 1 m 2 r 123

~r 12.

Where G is the gravitational constant

G = 6. 67 × 10 −^11 N · m^2 /kg.

Free-fall acceleration for objects near the surface of the earth:

g =

G ME

R^2 E

= 9.81 m/s^2.

Measurement of G: Torsion balance (first Cavendish 1798).

Derivation of Kepler’s Laws

Kepler’s first law: With a bit more involved mathematics than we have presently at our disposal, one can show that the only closed solutions to Newton’s two body force are elliptical orbits (intermediate mechanics for physicists).

Kepler’s second law: (Figure 11-8 of Tipler-Mosca.)

The area swept out by the radius vector ~r in the time dt is

dA =

|~r × ~v dt| =

2 m

|~r × m ~v| dt =

L

2 m

dt

where L = |~r × ~p| is the magnitude of the orbital angular momentum of the planet about the sun. Since the force on the planet is along the line from the planet to the center of the ellipse, there is no torque acting on the planet, and L is conserved. Therefore, dA dt

L

2 m

= constant.

Kepler’s third law:

We will show this for the special orbit of a circle. Then

F = G

m 1 m 2 r^2

= m 2 a = m 2

v^2 r

and

v^2 =

2 π r T

G m 1 r follows, which can be written as Kepler’s third law:

T 2 =

4 π^2 G m 1

r^3.

Escape Speed

Initial kinetic energy needed to escape from the earth’ surface to r = ∞:

0 = Ki + Ui =

m v e^2 − G

ME m RE

where ve is called escape speed. Solving for ve:

ve =

2 G ME

RE

2 g RE.

ve =

2 (9.81 m/s^2 ) (6. 37 × 106 m) = 11.2 km/s.

If E = Ki + Ui < 0 the system is bound. If E = Ki + Ui ≥ 0 the system is unbound.

Gravitational field (of the earth):

~g =

F~

m

G ME

r^2