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Gravity

Newton’s Law of Gravitation
Kepler’s Laws of Planetary
          Motion
    Gravitational Fields
Newton’s Law of Gravitation
                               r                            m2

   m1

 There is a force of gravity between any pair of objects
 anywhere. The force is proportional to each mass and
 inversely proportional to the square of the distance between
 the two objects. Its equation is:
                            G m1 m2
                     FG   =    r2
The constant of proportionality is G, the universal gravitation
constant. G = 6.67 · 10-11 N·m2 / kg2. Note how the units of G all
cancel out except for the Newtons, which is the unit needed on the
left side of the equation.
Gravity Example
How hard do two planets pull on each other if their masses are
1.23 × 1026 kg and 5.21 × 1022 kg and they 230 million kilometers
apart?
                 G m1 m2
         FG =        r2
             (6.67 · 10-11 N·m2 / kg2) (1.23 · 1026 kg) (5.21 · 1022 kg)
         =
                              (230 · 103 · 106 m) 2
         = 8.08 · 1015 N

This is the force each planet exerts on the other. Note the
denominator is has a factor of 103 to convert to meters and a factor of
106 to account for the million. It doesn’t matter which way or how
fast the planets are moving.
3rd Law: Action-Reaction
In the last example the force on each planet is the same. This is due to
to Newton’s third law of motion: the force on Planet 1 due to Planet 2
is just as strong but in the opposite direction as the force on Planet 2
due to Planet 1. The effects of these forces are not the same, however,
since the planets have different masses.
For the big planet: a = (8.08 · 1015 N) / (1.23 · 1026 kg)
                     = 6.57 · 10-11 m/s2.

For the little planet: a = (8.08 · 1015 N) / (5.21 · 1022 kg)
                        = 1.55 · 10-7 m/s2.


   5.21    8.08 · 1015 N                     8.08 · 1015 N
                                                                1.23 · 1026 kg
 · 1022 kg
Inverse Square Law
 The law of gravitation is called an inverse square law because the
 magnitude of the force is inversely proportional to the square of the
 separation. If the masses are moved twice as far apart, the force of
 gravity between is cut by a factor of four. Triple the separation and
 the force is nine times weaker.

                             G m1 m2
                      FG   =    r2


What if each mass and the separation were all quadrupled?

    answer:       no change in the force
Calculating the Gravitational Constant
In 1798 Sir Henry Cavendish suspended a rod with two small masses
(red) from a thin wire. Two larger mass (green) attract the small
masses and cause the wire to twist slightly, since each force of
attraction produces a torque in the same direction. By varying the
masses and measuring the separations and the amount of twist,
Cavendish was the first to calculate G.



                                            Since G is only
                                            6.67 · 10-11 N·m2 / kg2,
                                            the measurements had
                                            to be very precise.
Calculating the mass of the Earth
 Knowing G, we can now actually calculate the mass of the Earth.
 All we do is write the weight of any object in two different ways and
 equate them. Its weight is the force of gravity between it and the
 Earth, which is FG in the equation below. ME is the mass of the
 Earth, RE is the radius of the Earth, and m is the mass of the object.
 The object’s weight can also be written as mg.
                  G m1 m2          G ME m
           FG   =    r2
                               =    RE 2
                                              = mg

The m’s cancel in the last equation. g can be measured experimentally;
Cavendish determined G’s value; and RE can be calculated at
6.37 · 106 m (see next slide). ME is the only unknown. Solving for
ME we have:
                       g RE 2
               ME =           = 5.98 · 1024 kg
                         G
Calculating the radius of the Earth
This is similar to the way the Greeks approximated Earth’s radius over
2000 years ago:
                               θ
                                  Red pole blocks incoming solar rays
                                  and makes a shadow. θ is measured.
                      RE
                              s
                       θ
                                    The green pole is on the same
                                    meridian as the red one, but it casts
              Earth                 no shadow at this latitude. s is the
                                    measured distance between the
                                    cities in which the poles stand.

             θ is also the central angle of the arc. s = RE θ
                           RE = s / θ ≈ 6.37 · 106 m
Net Force Gravity Problem
    3 × 106 kg                 3 asteroids are positioned as shown,
                               forming a right triangle. Find the net
40 m                           force on the 2.5 million kg asteroid.

    2.7 × 106 kg                   2.5 × 106 kg
                 60 m
Steps:
1. Find each force of gravity on it and draw in the vectors.
2. Find the angle at the lower right.
3. One force vector is to the left; break the other one down into
   components.
4. Find the resultant vector: magnitude via Pythagorean theorem;
   direction via inverse tangent.
         answer:        0.212 N at 14.6° above horizontal (N of W)
Falling Around                                x = vt
                                                    v
the Earth              y = 0.5 g t 2 {



                               Newton imagined a cannon ball fired
                        horizontally from a mountain top at a speed
                  v. In a time t it falls a distance y = 0.5 g t 2 while

                moving horizontally a distance x = v t. If fired fast
            enough (about 8 km/s), the Earth would curve downward
         the same amount the cannon ball falls downward. Thus, the
      projectile would never hit the ground, and it would be in orbit.
     The moon “falls” around Earth in the exact same way but at a
    much greater altitude.                                          .
                                             continued on next slide
Necessary Launch Speed for Orbit
R = Earth’s radius                            x 2 + R 2 = (R + y) 2
t = small amount of time after launch
x = horiz. distance traveled in time t         = R2 + 2 R y + y 2
y = vertical distance fallen in time t
                                                Since y << R,
    (If t is very small, the red
    segment is nearly vertical.)              x 2 + R2 ≈ R2 + 2 R y
                                                 ⇒ x2 ≈ 2R y
                  x = vt                    ⇒ v 2 t 2 ≈ 2 R (g t 2 / 2)
y = gt 2 / 2
                                             ⇒ v 2 ≈ R g.        So,
                                         v ≈ (6.37 · 106 m · 9.8 m/s2) ½
                   R       R
                                                 v ≈ 7900 m/s
Early Astronomers
In the 2nd century AD the Alexandrian astronomer Ptolemy put forth a
theory that Earth is stationary and at the center of the universe and that
the sun, moon, and planets revolve around it. Though incorrect, it was
accepted for centuries.
                 In the early 1500’s the Polish astronomer Nicolaus
                 Copernicus boldly rejected Ptolemy’s geocentric model
                 for a heliocentric one. His theory put the sun stated that
                 the planets revolve around the sun in circular orbits and
                 that Earth rotates daily on its axis.
                 In the late 1500’s the Danish astronomer Tycho Brahe
                 made better measurements of the planets and stars than
                 anyone before him. The telescope had yet to be
                 invented. He believed in a Ptolemaic-Coperican
                 hybrid model in which the planets revolve around the
                 sun, which in turn revolves around the Earth.
Early Astronomers
Both Galileo and Kepler contributed greatly to work of the English
           scientist Sir Isaac Newton a generation later.
              In the late 1500’s and early 1600’s the Italian scientist
              Galileo was one of the very few people to advocate the
              Copernican view, for which the Church eventually had
              him placed under house arrest. After hearing about the
              invention of a spyglass in Holland, Galileo made a
              telescope and discovered four moons of Jupiter, craters
              on the moon, and the phases of Venus.
              The German astronomer Johannes Kepler was a
              contemporary of Galileo and an assistant to Tycho
              Brahe. Like Galileo, Kepler believed in the heliocentric
               system of Copernicus, but using Brahe’s planetary data
              he deduced that the planets move in ellipses rather than
              circles. This is the first of three planetary laws that
              Kepler formulated based on Brahe’s data.
Kepler’s Laws of
                 Planetary Motion
           Here is a summary of Kepler’s 3 Laws:

1. Planets move around the sun in elliptical paths with the
   sun at one focus of the ellipse.
2. While orbiting, a planet sweep out equal areas in equal
   times.
3. The square of a planet’s period (revolution time) is
   proportional to the cube of its mean distance from the sun:

   T 2 ∝These laws apply to any satellite orbiting a much
         R3
                          larger body.
Kepler’s First Law
   Planets move around the sun in elliptical paths with the
              sun at one focus of the ellipse.


                       F1                       F2

                      Sun

                                                  P
                                                      Planet
An ellipse has two foci, F1 and F2. For any point P on the ellipse,
F1 P + F2 P is a constant. The orbits of the planets are nearly circular
(F1 and F2 are close together), but not perfect circles. A circle is a an
ellipse with both foci at the same point--the center. Comets have very
eccentric (highly elliptical) orbits.
Kepler’s Second Law                     (proven in advanced physics)
While orbiting, a planet sweep out equal areas in equal times.

              A

                                                             D

                       Sun                                   C

             B

 The blue shaded sector has the same area as the red shaded sector.
 Thus, a planet moves from C to D in the same amount of time as it
 moves from A to B. This means a planet must move faster when it’s
 closer to the sun. For planets this affect is small, but for comets it’s
 quite noticeable, since a comet’s orbit is has much greater eccentricity.
Kepler’s Third Law
      The square of a planet’s period is proportional to the
        cube of its mean distance from the sun: T 2 ∝ R 3
Assuming that a planet’s orbit is circular (which is not exactly correct
but is a good approximation in most cases), then the mean distance
from the sun is a constant--the radius. F is the force of gravity on the
planet. F is also the centripetal force. If the orbit is circular, the
planet’s speed is constant, and v = 2 π R / T. Therefore,
                            GMm          m v2   m [2 π R / T] 2
                                       =      =
                             R2           R         R
                 m              Cancel m’s      GM       4 π2 R
             F    Planet        and simplify:         =
                                                 R2        T2
     M
             R                                    4 π2 3
    Sun                         Rearrange: T 2 =      R
                                                 GM
                     Since G, M, and π are constants, T 2 ∝ R 3.
Third Law Analysis
                                               4 π2 3
                    We just derived T 2 =           R
                                              GM
• It also shows that the orbital period depends on the mass of the
central body (which for a planet is its star) but not on the mass of the
orbiting body. In other words, if Mars had a companion planet the
same distance from the sun, it would have the same period as Mars,
regardless of its size.
• This shows that the farther away a planet is from its star, the longer it
takes to complete an orbit. Likewise, an artificial satellite circling
Earth from a great distance has a greater period than a satellite orbiting
closer. There are two reasons for this: 1. The farther away the satellite
is, the farther it must travel to complete an orbit; 2. The farther out its
orbit is, the slower it moves, as shown:
           GMm             m v2                  GM
                       =             ⇒ v=
              R2            R                      R
Third Law Example
One astronomical unit (AU) is the distance between Earth and the
sun (about 93 million miles). Jupiter is 5.2 AU from the sun. How
long is a Jovian year?
answer: Kepler’s 3rd Law says T 2 ∝ R 3, so T 2 = k R 3, where k is
the constant of proportionality. Thus, for Earth and Jupiter we have:

                  TE 2 = k RE 3 and TJ 2 = k RJ 3
k’s value matters not; since both planets are orbiting the same
central body (the sun), k is the same in both equations. TE = 1 year,
and
RJ / RE = 5.2, so 3
                  dividing equations:
    TJ  2
           RJ
         =             ⇒      TJ 2 = (5.2) 3   ⇒ TJ = 11.9 years
    TE 2
           RE 3
                                                  continued on next slide
Third Law Example                (cont.)
What is Jupiter’s orbital speed?
answer: Since it’s orbital is approximately circular, and it’s speed
is approximately constant:           Jupiter is 5.2 AU from the sun
                                      (5.2 times farther than Earth is).

 v=
    d
           = 2 π (5.2) (93 · 106 miles) 1 year       1 day
    t                                  ·          ·
                    11.9 years           365 days   24 hours

≈ 29,000 mph.                           Jupiter’s period from last slide

This means Jupiter is cruising through the solar system at about
13,000 m/s ! Even at this great speed, though, Jupiter is so far away
that when we observe it from Earth, we don’t notice it’s motion.
Planets closer to the sun orbit even faster. Mercury, the closest
planet, is traveling at about 48,000 m/s !
Third Law Practice Problem
 Venus is about 0.723 AU from the sun, Mars
  1.524 AU. Venus takes 224.7 days to circle
the sun. Figure out how long a Martian year is.


     answer:     686 days
Uniform Gravitational Fields
We live in what is essentially a uniform gravitational field. This means
that the force of gravity near the surface of the Earth is pretty much
constant in magnitude and direction. The green lines are gravitational
field lines. They show the direction of the gravitational force on any
object in the region (straight down). In a uniform field, the lines are
parallel and evenly spaced. Near Earth’s surface the magnitude of the
gravitational field is 9.8 N / kg. That is, every kilogram of mass an
object has experiences 9.8 N of force. Since a Newton is a kilogram ·
meter per second squared, 1 N / kg = 1 m/s2. So, the gravitational field
strength is just the acceleration due to gravity, g.
                                                   continued on next slide




                            Earth’s surface
Uniform Gravitational Fields             (cont.)
A 10 kg mass is near the surface of the Earth. Since the field
strength is 9.8 N / kg, each of the ten kilograms feels a 9.8 N
force, for a total of 98 N. So, we can calculate the force of
gravity by multiply mass and field strength. This is the
same as calculating its weight (W = mg).




                      10 kg

             98 N

                               Earth’s surface
Nonuniform Gravitational Fields
Near Earth’s surface the gravitational field is approximately uniform.
Far from the surface it looks more like a sea urchin.

                                          The field lines
                                          • are radial, rather than
                                            parallel, and point toward
                                            center of Earth.
                                          • get farther apart farther from
                Earth                      the surface, meaning the
                                           field is weaker there.
                                          • get closer together closer to
                                            the surface, meaning the
                                            field is stronger there.

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Chap8

  • 1. Gravity Newton’s Law of Gravitation Kepler’s Laws of Planetary Motion Gravitational Fields
  • 2. Newton’s Law of Gravitation r m2 m1 There is a force of gravity between any pair of objects anywhere. The force is proportional to each mass and inversely proportional to the square of the distance between the two objects. Its equation is: G m1 m2 FG = r2 The constant of proportionality is G, the universal gravitation constant. G = 6.67 · 10-11 N·m2 / kg2. Note how the units of G all cancel out except for the Newtons, which is the unit needed on the left side of the equation.
  • 3. Gravity Example How hard do two planets pull on each other if their masses are 1.23 × 1026 kg and 5.21 × 1022 kg and they 230 million kilometers apart? G m1 m2 FG = r2 (6.67 · 10-11 N·m2 / kg2) (1.23 · 1026 kg) (5.21 · 1022 kg) = (230 · 103 · 106 m) 2 = 8.08 · 1015 N This is the force each planet exerts on the other. Note the denominator is has a factor of 103 to convert to meters and a factor of 106 to account for the million. It doesn’t matter which way or how fast the planets are moving.
  • 4. 3rd Law: Action-Reaction In the last example the force on each planet is the same. This is due to to Newton’s third law of motion: the force on Planet 1 due to Planet 2 is just as strong but in the opposite direction as the force on Planet 2 due to Planet 1. The effects of these forces are not the same, however, since the planets have different masses. For the big planet: a = (8.08 · 1015 N) / (1.23 · 1026 kg) = 6.57 · 10-11 m/s2. For the little planet: a = (8.08 · 1015 N) / (5.21 · 1022 kg) = 1.55 · 10-7 m/s2. 5.21 8.08 · 1015 N 8.08 · 1015 N 1.23 · 1026 kg · 1022 kg
  • 5. Inverse Square Law The law of gravitation is called an inverse square law because the magnitude of the force is inversely proportional to the square of the separation. If the masses are moved twice as far apart, the force of gravity between is cut by a factor of four. Triple the separation and the force is nine times weaker. G m1 m2 FG = r2 What if each mass and the separation were all quadrupled? answer: no change in the force
  • 6. Calculating the Gravitational Constant In 1798 Sir Henry Cavendish suspended a rod with two small masses (red) from a thin wire. Two larger mass (green) attract the small masses and cause the wire to twist slightly, since each force of attraction produces a torque in the same direction. By varying the masses and measuring the separations and the amount of twist, Cavendish was the first to calculate G. Since G is only 6.67 · 10-11 N·m2 / kg2, the measurements had to be very precise.
  • 7. Calculating the mass of the Earth Knowing G, we can now actually calculate the mass of the Earth. All we do is write the weight of any object in two different ways and equate them. Its weight is the force of gravity between it and the Earth, which is FG in the equation below. ME is the mass of the Earth, RE is the radius of the Earth, and m is the mass of the object. The object’s weight can also be written as mg. G m1 m2 G ME m FG = r2 = RE 2 = mg The m’s cancel in the last equation. g can be measured experimentally; Cavendish determined G’s value; and RE can be calculated at 6.37 · 106 m (see next slide). ME is the only unknown. Solving for ME we have: g RE 2 ME = = 5.98 · 1024 kg G
  • 8. Calculating the radius of the Earth This is similar to the way the Greeks approximated Earth’s radius over 2000 years ago: θ Red pole blocks incoming solar rays and makes a shadow. θ is measured. RE s θ The green pole is on the same meridian as the red one, but it casts Earth no shadow at this latitude. s is the measured distance between the cities in which the poles stand. θ is also the central angle of the arc. s = RE θ RE = s / θ ≈ 6.37 · 106 m
  • 9. Net Force Gravity Problem 3 × 106 kg 3 asteroids are positioned as shown, forming a right triangle. Find the net 40 m force on the 2.5 million kg asteroid. 2.7 × 106 kg 2.5 × 106 kg 60 m Steps: 1. Find each force of gravity on it and draw in the vectors. 2. Find the angle at the lower right. 3. One force vector is to the left; break the other one down into components. 4. Find the resultant vector: magnitude via Pythagorean theorem; direction via inverse tangent. answer: 0.212 N at 14.6° above horizontal (N of W)
  • 10. Falling Around x = vt v the Earth y = 0.5 g t 2 { Newton imagined a cannon ball fired horizontally from a mountain top at a speed v. In a time t it falls a distance y = 0.5 g t 2 while moving horizontally a distance x = v t. If fired fast enough (about 8 km/s), the Earth would curve downward the same amount the cannon ball falls downward. Thus, the projectile would never hit the ground, and it would be in orbit. The moon “falls” around Earth in the exact same way but at a much greater altitude. . continued on next slide
  • 11. Necessary Launch Speed for Orbit R = Earth’s radius x 2 + R 2 = (R + y) 2 t = small amount of time after launch x = horiz. distance traveled in time t = R2 + 2 R y + y 2 y = vertical distance fallen in time t Since y << R, (If t is very small, the red segment is nearly vertical.) x 2 + R2 ≈ R2 + 2 R y ⇒ x2 ≈ 2R y x = vt ⇒ v 2 t 2 ≈ 2 R (g t 2 / 2) y = gt 2 / 2 ⇒ v 2 ≈ R g. So, v ≈ (6.37 · 106 m · 9.8 m/s2) ½ R R v ≈ 7900 m/s
  • 12. Early Astronomers In the 2nd century AD the Alexandrian astronomer Ptolemy put forth a theory that Earth is stationary and at the center of the universe and that the sun, moon, and planets revolve around it. Though incorrect, it was accepted for centuries. In the early 1500’s the Polish astronomer Nicolaus Copernicus boldly rejected Ptolemy’s geocentric model for a heliocentric one. His theory put the sun stated that the planets revolve around the sun in circular orbits and that Earth rotates daily on its axis. In the late 1500’s the Danish astronomer Tycho Brahe made better measurements of the planets and stars than anyone before him. The telescope had yet to be invented. He believed in a Ptolemaic-Coperican hybrid model in which the planets revolve around the sun, which in turn revolves around the Earth.
  • 13. Early Astronomers Both Galileo and Kepler contributed greatly to work of the English scientist Sir Isaac Newton a generation later. In the late 1500’s and early 1600’s the Italian scientist Galileo was one of the very few people to advocate the Copernican view, for which the Church eventually had him placed under house arrest. After hearing about the invention of a spyglass in Holland, Galileo made a telescope and discovered four moons of Jupiter, craters on the moon, and the phases of Venus. The German astronomer Johannes Kepler was a contemporary of Galileo and an assistant to Tycho Brahe. Like Galileo, Kepler believed in the heliocentric system of Copernicus, but using Brahe’s planetary data he deduced that the planets move in ellipses rather than circles. This is the first of three planetary laws that Kepler formulated based on Brahe’s data.
  • 14. Kepler’s Laws of Planetary Motion Here is a summary of Kepler’s 3 Laws: 1. Planets move around the sun in elliptical paths with the sun at one focus of the ellipse. 2. While orbiting, a planet sweep out equal areas in equal times. 3. The square of a planet’s period (revolution time) is proportional to the cube of its mean distance from the sun: T 2 ∝These laws apply to any satellite orbiting a much R3 larger body.
  • 15. Kepler’s First Law Planets move around the sun in elliptical paths with the sun at one focus of the ellipse. F1 F2 Sun P Planet An ellipse has two foci, F1 and F2. For any point P on the ellipse, F1 P + F2 P is a constant. The orbits of the planets are nearly circular (F1 and F2 are close together), but not perfect circles. A circle is a an ellipse with both foci at the same point--the center. Comets have very eccentric (highly elliptical) orbits.
  • 16. Kepler’s Second Law (proven in advanced physics) While orbiting, a planet sweep out equal areas in equal times. A D Sun C B The blue shaded sector has the same area as the red shaded sector. Thus, a planet moves from C to D in the same amount of time as it moves from A to B. This means a planet must move faster when it’s closer to the sun. For planets this affect is small, but for comets it’s quite noticeable, since a comet’s orbit is has much greater eccentricity.
  • 17. Kepler’s Third Law The square of a planet’s period is proportional to the cube of its mean distance from the sun: T 2 ∝ R 3 Assuming that a planet’s orbit is circular (which is not exactly correct but is a good approximation in most cases), then the mean distance from the sun is a constant--the radius. F is the force of gravity on the planet. F is also the centripetal force. If the orbit is circular, the planet’s speed is constant, and v = 2 π R / T. Therefore, GMm m v2 m [2 π R / T] 2 = = R2 R R m Cancel m’s GM 4 π2 R F Planet and simplify: = R2 T2 M R 4 π2 3 Sun Rearrange: T 2 = R GM Since G, M, and π are constants, T 2 ∝ R 3.
  • 18. Third Law Analysis 4 π2 3 We just derived T 2 = R GM • It also shows that the orbital period depends on the mass of the central body (which for a planet is its star) but not on the mass of the orbiting body. In other words, if Mars had a companion planet the same distance from the sun, it would have the same period as Mars, regardless of its size. • This shows that the farther away a planet is from its star, the longer it takes to complete an orbit. Likewise, an artificial satellite circling Earth from a great distance has a greater period than a satellite orbiting closer. There are two reasons for this: 1. The farther away the satellite is, the farther it must travel to complete an orbit; 2. The farther out its orbit is, the slower it moves, as shown: GMm m v2 GM = ⇒ v= R2 R R
  • 19. Third Law Example One astronomical unit (AU) is the distance between Earth and the sun (about 93 million miles). Jupiter is 5.2 AU from the sun. How long is a Jovian year? answer: Kepler’s 3rd Law says T 2 ∝ R 3, so T 2 = k R 3, where k is the constant of proportionality. Thus, for Earth and Jupiter we have: TE 2 = k RE 3 and TJ 2 = k RJ 3 k’s value matters not; since both planets are orbiting the same central body (the sun), k is the same in both equations. TE = 1 year, and RJ / RE = 5.2, so 3 dividing equations: TJ 2 RJ = ⇒ TJ 2 = (5.2) 3 ⇒ TJ = 11.9 years TE 2 RE 3 continued on next slide
  • 20. Third Law Example (cont.) What is Jupiter’s orbital speed? answer: Since it’s orbital is approximately circular, and it’s speed is approximately constant: Jupiter is 5.2 AU from the sun (5.2 times farther than Earth is). v= d = 2 π (5.2) (93 · 106 miles) 1 year 1 day t · · 11.9 years 365 days 24 hours ≈ 29,000 mph. Jupiter’s period from last slide This means Jupiter is cruising through the solar system at about 13,000 m/s ! Even at this great speed, though, Jupiter is so far away that when we observe it from Earth, we don’t notice it’s motion. Planets closer to the sun orbit even faster. Mercury, the closest planet, is traveling at about 48,000 m/s !
  • 21. Third Law Practice Problem Venus is about 0.723 AU from the sun, Mars 1.524 AU. Venus takes 224.7 days to circle the sun. Figure out how long a Martian year is. answer: 686 days
  • 22. Uniform Gravitational Fields We live in what is essentially a uniform gravitational field. This means that the force of gravity near the surface of the Earth is pretty much constant in magnitude and direction. The green lines are gravitational field lines. They show the direction of the gravitational force on any object in the region (straight down). In a uniform field, the lines are parallel and evenly spaced. Near Earth’s surface the magnitude of the gravitational field is 9.8 N / kg. That is, every kilogram of mass an object has experiences 9.8 N of force. Since a Newton is a kilogram · meter per second squared, 1 N / kg = 1 m/s2. So, the gravitational field strength is just the acceleration due to gravity, g. continued on next slide Earth’s surface
  • 23. Uniform Gravitational Fields (cont.) A 10 kg mass is near the surface of the Earth. Since the field strength is 9.8 N / kg, each of the ten kilograms feels a 9.8 N force, for a total of 98 N. So, we can calculate the force of gravity by multiply mass and field strength. This is the same as calculating its weight (W = mg). 10 kg 98 N Earth’s surface
  • 24. Nonuniform Gravitational Fields Near Earth’s surface the gravitational field is approximately uniform. Far from the surface it looks more like a sea urchin. The field lines • are radial, rather than parallel, and point toward center of Earth. • get farther apart farther from Earth the surface, meaning the field is weaker there. • get closer together closer to the surface, meaning the field is stronger there.