Ch 7: Universal Gravitation

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Barry Latham Honors Physics Bloom High School. Ch 7: Universal Gravitation. 7.1: Kepler’s Laws of Motion. Based on years of observations, Kepler devised a series of laws known to us as his “Laws of Planetary Motion.” - PowerPoint PPT Presentation

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CH 7: UNIVERSAL GRAVITATION

Barry LathamHonors PhysicsBloom High School

7.1: Kepler’s Laws of Motion

Based on years of observations, Kepler devised a series of laws known to us as his “Laws of Planetary Motion.”

1st Law: The path of each planet about the sun is an ellipse with the sun at the focus.

2nd Law: Each planet moves so that an imaginary line drawn from the sun to the planet sweeps out equal areas in equal periods of time.

3rd Law: The ratio of the squares of the periods T of any two planets revolving about the sun is equal to the ratio of the cubes of their mean distances s to the sun: (T1/T2)2=(s1/s2)3.

Kepler’s Laws

Problem Solving

As always, picture/data/formula/algebra! Keep the unknown as a numerator Rearrange the formula BEFORE you plug

the values in. Watch parenthesis, squares, cubes and

their roots. Recall that: x½ = 2√(x) x1/3 =

3√(x)x2/3 = 3√(x2) x3/2 =

2√(x3)

Distance to Mars?

According to Kepler, Mars’ “year” is 687 Earth-days. Using what we know about the distance and period of the earth, we can find Mars’ distance. The mean distance of the Earth to the Sun is 1.50x1011 m.

Picture/Data/Formula/Algebra (T1/T2)2=(s1/s2)3

T1=Mars=687 days s1=Mars’ orbital radius T2=Earth=365.24 days s2=Earth orbital radius=

1.50x1011 m (687 days/365.24 days)2=(s1/1.50x1011 m)3

(1.5x1011 m)(687 days/365.24 days)2/3=s1 s1=2.28x1011 m

Newton’s Law of Universal Gravitation Every particle in the universe attracts

every other particle with a force that is proportional to the product of their masses and inversely proportional to the square of the distance between them. This force acts along the line joining the two particles.

F=Gm1m2/r2

Universal Gravitation Equation

F=Gm1m2/r2

F= the force of gravity (in Newton’s) m1 & m2= the two individual masses that we are

measuring r= the distance between the masses, measured in a

straight line and using their center of mass G= the universal gravitation constant

6.67x10-11 N m2/kg2

F=(N m2/kg2)(kg)(kg)/(m)2

F=N (big surprise)

The Romance of Gravity Find the force of attraction between two people. A 74

kg person is sitting 1.2 m away from a 84 kg person at a lab bench. Estimate the force attracting them together.

Picture/Data/Formula/Algebra F=Gm1m2/r2

G= 6.67x10-11 N m2/kg2

m1=74 kg m2=84 kg r=1.2 m F=G(74 kg)(84 kg)/(1.2 m)2

F= 2.879x10-7 N (equal to a 0.03 mg object)

Less Romantic Gravity, part 1

As you get far away from Earth, does your weight decrease?

What is the weight of a 2000kg satellite when it is in the lab at NASA?

Fg=mg Fg=(2000 kg)(9.80 m/s2) Fg=19,600 N

Less Romantic Gravity, part 2

What is the force of gravity acting on a 2000 kg satellite when it orbits two Earth radii from the Earth’s center (rEarth = 6.38x106 m).

F=Gm1m2/r2

F=G(2000 kg)(5.97x1024 kg)/(2x6.38x106 m)2

Fg=4,891 N

This is 1/4th of what it was in the lab!

Universal Gravitation &Kepler’s 3rd Law

If we take Newton’s law of universal gravitation, F=Gm1m2/r2

And Kepler’s 3rd Law (with centripetal acceleration included) F=m4p2r/T2

m=mass of central body T=period of orbit (time of one revolution)

Set them equal (they are both F) and solve for T T=√(r3(4p2)/(Gm)) This represents the time it takes for an object to go

around a central body one time.

Cavendish’s Device

Using a device shown to the right, Cavendish was able to accurately measure the force of gravity.

By twisting the string slightly, the scale displayed the force of attraction between the sphere on the rod and sphere A.

Geophysical Applications

When discussing objects on the earth’s surface, m1 becomes mE and r is the radius of the earth (rE).

Original formula F=Gm1m2/r2

substituted m2 g for F m2g=GmEm2/rE2

cancel m2 g=GmE/rE2

So the acceleration due to gravity of an object is dependant upon the mass of the object and the radius of the object (in this case, the earth)

In lieu of Earth, we can use the data from any object!

What’s the mass of Earth?

Unless you have a HUGE scale, we need another way to determine it.

g=GmE/rE2 but solve for mE

mE=g rE2/G

mE=(9.80 m/s2)(6.38x106 m)2/(6.67x10-11 N m2/kg2)

mE=5.98x1024 kg

Is “g” really 9.8?

Find g at sea level on Earth.

g=GmE/rE2

g=(6.67x10-11 N m2/kg2)(5.98x1024 kg)/(6.38x106 m)2

g=9.79909 m/s2

So, yes, it’s basically 9.8.

Is “g” really 9.8?

Gravity at the top of Mt. Everest. Mt. Everest has a height of 8,850 m above sea level.

g=GmE/rE2

g=(6.67x10-11 N m2/kg2)(5.98x1024 kg)/(6.38x106 m + 8,850 m)2

g=9.77195 m/s2

So, yes, it’s basically still 9.8.

Is g 9.8 everywhere on Earth?

Explain the losses or gains in gravity.

HW p. 178 q. 6-10

7.2: Satellites

Artificial satellites are put into orbit with three different final velocities. Circular orbit (space shuttles)

27,000 km/h Elliptical orbit

30,000 km/h If an object needs to leave

earth’s orbit, such as solar probes, and extra-solar objects 40,000 km/h

Satellite Orbital Velocity

Geostationary satellite (communications & weather) Stays above the same point on earth

Satellite Equation Derivation

To remain above the same point, the satellite must have a period (T) of one day (one cycle per day).

Apply Newton’s Second law and a new formula (centripetal acceleration) Assume the orbit is circular (which it pretty much is)

The only force on the satellite is the force of universal gravitation. Plug our new gravity equation and centripetal acceleration into F=ma.

F=ma F=Gm1m2/r2 ac=v2/r

GmsatmE/r2=(msat)(v2/r)

Speed (v) of a Satellite Orbiting a Central Body in Circular Orbit

Since the satellite revolves around the earth at the same rate the earth turns, v=2pr/T T is the period of the movement, 1 day (86,400 s)

GmsatmE/r2=msatv2/rcancel msat and r GmE/r=v2 solve for v v=√(GmE/r) mE is the mass of the Earth

but can represent the central body

√((6.67x10-11)(5.98x1024)/(4.23x107))=3070 m/s

We find the same result if we use, v=2pr/T. v=2p (4.23x107)/(86,400)=3076 m/s

Period (T) of a Satellite Orbiting a Central Body in Circular Orbit

We saw this on Slide 11!

T=√(r3(4p2)/(Gm)) This represents the time it takes for an object to

go around a central body one time. If the mass (m) is Earth, then m=mE

Orbital height (r) of a Satellite Orbiting a Central Body in Circular Orbit

Using any number of equations containing r, we can find the orbital height Remember that height is from the center of the central object to

the center of the satellite

F=Gm1m2/r2 Newton’s Universal Gravitation r= √( Gm1m2/F)

F=m4p2r/T2 Kepler’s Third Law r=FT2/(m4p2)

T= 2p√(r3/(Gm)) Newton’s version of Kepler’s 3rd Law r=

v=√(GmE/r) v of satellite in circular orbit r=GmE/v2

Inertial Mass

According to F=ma, the mass of an object is the relationship between the Force applied and the acceleration of the object.

Because every object with mass has inertia, we can rearrange and use subscripts. minertia=Fnet/a

More mass means less reaction to the same force Inertial mass is independent of location or a

reference body It’s how they measure the astronauts mass in space!

Lab 7-2

Gravitational Mass

Unlike Inertial Mass, gravitational mass is dependant on a reference material (sometime a whole planet!)

Using Newton’s Universal Gravitation formula, we can rearrange to find the mass of an object Fgrav=GmgravmE/r2

mgrav=r2Fgrav/(GmE) To measure this, we use a triple beam or

digital balance in the presence of gravity

Relativity & Gravity

According to Einstein, gravity is not a force, but an effect of space itself

Mass causes space to curve, so objects are pulled toward the “dimple” in space-time (even light)

Larger objects make larger “dimples” hence larger gravitational pull

Earth’s gravitational field distorting space-time

Blackholes, defined

Black hole- a concentration of mass so dense that nothing can escape the pull of it’s gravity, not even light Formed by the severe gravitational pull overcoming the

thermonuclear reaction pushing the material out Black hole formation

http://www.youtube.com/watch?v=jT2wkbPfUYc http://www.youtube.com/watch?v=UkospV4Gya8&feature=related

Size? Black holes can be measured by mass or area Mass- 1031 to 1036 kg (10-1,000,000 times as massive as our Sun) Volume- based on Schwartzchild radius or radius of the horizon

A black hole with a mass the same as the Sun would be 3 km in radius The Sun has a radius of 700,000 km now!

A 10-solar-mass black hole would be 30km and so on Event Horizon- the point of no return, the Schwartzchild radius

Black Holes evaporate?

Black Holes will not eventually suck up everything in the universe

They emit “Hawking radiation” At the Event Horizon, a particle-antiparticle

pair can appear from within the black hole One particle gets sucked back in, the other

escapes Momentum & Energy are conserved The emitted particle is detected This happens so frequently, it is observed as a

matter/energy stream

Hawking Radiation

Black Hole Images

A wormhole

End of Unit Review, 1

What would make you weigh more: an earth twice as massive with the same diameter or one having half its diameter with the same mass?

Solution: Find out using F=Gm1m2/r2

Fg1=GmEmyou/rE2 normally, what is your Fg?

Fg2=G(2mE)myou/rE2 now, what is your Fg?

Fg3=GmEmyou/(½rE)2now, what is your Fg?

How do they all compare?

End of Unit Review, 2

Would one need a longer rocket to take off from the moon vs. earth?

What is needed to escape the Earth? The Moon? Gravity holds us in place, so which has less gravity?

Solution: Find out using g=GmE/rE2

For earth, g=9. 79909 m/s2

For the Moon, g=GmM/rM2

g=G(7.349x1022 kg)/(1.738x106 m)2

g=1.62 m/s2

End of Unit Review, 3

Based on our prior work, what would your weight be on the Moon?

FgE=m(9. 80 m/s2) FgM=m(1.62 m/s2)

FgE=(84.1 kg)(9. 80 m/s2)=824 N FgM=(84.1 kg)(1.62 m/s2)=136 N

End of Unit Review, 4

If an astronaut was to break the connection rope between him and the space shuttle, will gravity quickly pull him back to the shuttle? F=Gm1m2/r1-2

2

g=Gm/r2

What happens to the acceleration of an asteroid as it approaches a planet? If g based on distance? g=Gm/r2