The gravitational force between two objects is, Exercises of Physics

The gravitational force between two objects is proportional to their masses and inversely proportional to the square of the distance between their centers. G m.

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Recap: Newton’s Gravitational Law
The gravitational force between two objects is
proportional to their masses and inversely
proportional to the square of the distance
between their centers.
G m1 m2
r 2
F = (Newtons)
F is an attractive force vector acting along line
joining the two centers of masses.
G = Universal Gravitational
Constant
G = 6.67 x 10-11 N.m2/kg2
Note: G was not measured until > 100 years
after Newton! - by Henry Cavendish (18th cen.)
F1F2
r
m2
(F1 = -F2)
m1
(very
small)
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13

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Recap: Newton’s Gravitational Law

The gravitational force between two objects is

proportional to their masses and inversely

proportional to the square of the distance

between their centers.

G m

1

m

2

r

2

F =

(Newtons)

  • F is an attractive force vector acting along line

joining the two centers of masses.

  • G = Universal Gravitational

Constant

G = 6.67 x 10

- 11

N.m

2

/kg

2

Note: G was not measured until > 100 years

after Newton! - by Henry Cavendish (

th

cen.)

F

1

F

2

r

m

2

(F 1

= -F 2

)

m

1

(very

small)

m

How is Weight Related to Gravitation?

Gravitational force of attraction:

F (^) F

m

e

r

e

m

e

= mass of Earth = 5.98 x 10

24

kg

r

e

= radius of Earth = 6370 km

m = mass of an object

G m

e

m

r

e

2

if m = 150 kg, F = 1472 N (or ~ 330 lbs wt)

By Newton’s 2

nd

law (F=ma) we can also calculate weight:

W = m g = 9.81 x 150 = 1472 N

By equating these expressions for gravitational force:

m g = (^) or at surface: g =

G m

e

r

e

2

G m

1

m

2

r

2

F =

(N)

Result: ‘g’ is independent of mass of object !!

But this force creates the object’s weight:

F

F

m

2

m

1

r

2

  • Newton’s 3

rd

law: Each

body feels same force

acting on it (but

in opposite directions)

Gm

1

m

2

r

2

F=

  • Thus each body experiences an acceleration!

Example: Boy 40 kg jumps off a box:

Force on boy: F = m g = 40 x 9.81 = 392 N

Force on Earth: F = m

e

a = 392 N

5.98 x 10

24

or a = = 6.56 x 10

m/s

2

ie. almost zero!

Example: 3 billion people jumping off boxes all at same time

(mass 100 kg each)

Conclusion: The Earth is so massive, we have essentially

no effect on its motion!

3 x 10

9

x 100 x 9.

5.98 x 10

24

= 5 x 10

m/s

2

a =

Planetary Motions & Orbits (Chapter 5)

  • Heavenly bodies: sun, planets, stars… How planets move?

Greeks:

  • Stars remain in the same relative position to one another as

they move across the sky.

  • Several bright “stars” exhibit motion relative to other stars.
  • Bright “ wanderers ” called planets.
  • Planets roam in regular but curious manner.

Hypothesis:

  • Geocentric “Earth-centered” universe!
  • Sun moves around the Earth - like on a long rope with

Earth at its center.

  • Stars – lying on a giant sphere with Earth at center.
  • Moon too – exhibits phases as it orbits Earth.

Heliocentric Model: Copernicus (

th

century)

  • Sun centered view that was later proven by Galileo – using

telescope observations of Jupiter and its satellite moons.

  • Bad news : demoted Earth to status of just another planet!
  • Revolutionary concept – required the Earth to spin (to

explain Sun’s motion).

  • If Earth spinning why are we not thrown off? (at 1000 mph).
  • Good news : no more need for complex epicycles to explain

retrograde motion!

Result: Earth moves faster in orbit and Mars appears

to move backwards at certain times.

Earth orbit

Mars orbit

Same

direction

Fixed

stars

field

  • Copernicus heliocentric model assumed circular orbits – but

careful observations by Tycho Brahe (the last great “naked

eye” astronomer) showed not true…

  • Kepler (

th

century, Brahe’s student) developed three laws

based on emperical analysis of Brahe’s extensive data…

1. Orbits of planets around the sun are ellipses with

Sun at one focus.

two foci

Sun

planet

Note: A circle is a special

case of an ellipse with 2

foci coincident.

In reality, the planets’ orbits are very close to

circular but nevertheless are slightly elliptical.

  • This means that the “outer” planets (i.e. further from the

Sun than Earth) all have much larger orbital periods than

Earth (and vice versa).

i.e. Τ

2

r

3

  • So if we know Τ (by observations) we can find “r” for each

planet!

Conclusion:

  • These careful observations and new formula set the scene for

Newton’s theory of gravitation…

G m

1

m

2

r

2

F =

  • Using Kepler’s 3

rd

law , Newton calculated:

where: m = mass of Sun for the planetary motions, but

m = mass of Earth for the Moon’s motion.

  • Hence Kepler’s different result for the constant

for moon compared with other planets!

constant (fora given 'm' )

G m

4 D

r

Ô

2

3

2

2

r

3

= a constant number

equator

Example: Geosynchronous Orbit

  • Orbital period = 24 hours
  • Permits satellites to remain “stationary” over a given

equatorial longitude.

For Τ = 24 hrs

=> r = 42,000 km (to center Earth)

i.e. altitude ≈7 R

e

(compared with 60 R

e

for Moon.)

  • Geostationary orbit is very important for Earth observing and

communications satellites – a very busy orbit!

  • In general there are many, many possible orbits, e.g.:
    • Circular and elliptical
    • Low Earth orbits (LEO)
    • Geostationary orbit
    • Polar orbit
    • e.g. GPS system uses many

orbiting satellites.

circular

elliptical

polar

  • We can equate centripetal force to gravitational

attraction force to determine orbital speed (v

or

For circular motion:

Centripetal force = gravitational force (F

C

= F

G

2

2

or

r

G M m

r

m v

=

Orbital Velocity

M = planet’s mass

m = satellite’s mass

M » m

r

G M

v or

=

Results:

  • Any satellite regardless of its mass (provided M » m)

will move in a circular orbit or radius r and velocity v

or

  • The larger the orbital altitude, the lower the required

tangential velocity!

Qu: How to achieve orbit?

  • Launch vehicle rises initially vertical (minimum air drag).
  • Gradually rolls over and on separation of payload is moving

tangentially at speed v

or

produces circular orbit.

  • If speed less than v

or

, craft will

descend to Earth in an

(decaying) elliptical orbits.

  • If speed greater than v

or

it will

ascend into a large elliptical

orbit.

  • If speed greater than

it will escape earths gravity on

parabolic orbit!

Earth

circular (v

or

)

elliptical

parabolic

or

2v

  • Not a simple ellipse… due to gravitational force of

Earth and Sun.

  • Gravitational attraction between Earth and Moon provides

centripetal acceleration for orbit.

  • Sun’s gravitation distorts lunar orbital ellipse. (Orbit

oscillates about true elliptical path.)

Lunar Orbit

Sun

Moon

Earth 1.5 x 10

8

km

(≈ 400 R

moon

)

F ∝

r

2

  • Moon on same side of Earth as the Sun.
  • Essentially invisible (crescent moons seen

either side of New moon).

  • Rises at sunrise and sets at sunset (i.e. up all

day).

  • Solar eclipse condition.
  • At other times during moon’s orbit of Earth, we see

only a part of illuminated disk.

New moon:

  • When moon is in-between full and new phase, it can often

be seen during daylight too.

  • Example: half moon rises at noon and sets at midnight (and

vice versa).

  • Under good observing conditions (at sunset or sunrise) you

can see dark parts of moon illuminated by Earthshine!