Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits...
-
Upload
myron-moody -
Category
Documents
-
view
213 -
download
0
Transcript of Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits...
![Page 1: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/1.jpg)
Physics of AstronomyWinter Week 6 - Thus.16.Feb.2006
Astro-A: Universe 4 – Gravity and Orbits
Pre-lab – brief discussion
Astro-B: Finish C&O Ch.2
2:30 Seminar
4:00 Lab in CAL 1234
Let’s look at the sky together after lab!
Looking ahead (remember to take Universe Ch.4 online quiz)
![Page 2: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/2.jpg)
Astro-A: Universe 4 – Gravity & Orbits
Ptolemy: Circular orbits about Earth
Copernicus: Circular orbits about Sun
Kepler: Elliptical orbits about Sun
![Page 3: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/3.jpg)
We derived Kepler’s 3d law from Newton’s 2d law:
F=ma
Gravitational force acceleration in circular orbit
F=GmM/r2 a = v2/r
Solve for v2:
Speed v = distance/time = 2r/T. Plug this into v2 and solve for T2:
This is Kepler’s third law: T = period and r = orbit radius.
![Page 4: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/4.jpg)
For objects orbiting the Sun, Kepler’s law simplifies to a3 = p2,
where a=radius in AU and p=period in years
A satellite is placed in a circular orbit around the Sun, orbiting the Sun once every 10 months. How far is the satellite from the Sun? 2
3 2 10 a = p = _______
12
a ______
![Page 5: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/5.jpg)
Sidereal (real: P) and Synodic (apparent: S) periods:
A satellite is placed in a circular orbit around the Sun, orbiting the Sun once every 10 months. How often does the satellite pass between the Earth and the Sun?
1 1 1
'
1 1 1
1 1 110 1
121
________________
________________
sidereal period Earth s sidereal year synodic period
P E S
S
SS
![Page 6: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/6.jpg)
We can use Newton’s gravity to approximate the size of a black hole!
2
*
* ________grav
Energy Force distance
GmME r
r
Knowing the gravitational force between two bodies m and M, we can find their gravitational energy:
In order for an object (say, m) to escape M’s gravity,
It needs sufficient kinetic energy K=1/2 mv2 …
![Page 7: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/7.jpg)
Use energy conservation to find the size of R of a black hole:
21
2____________
Gravitational energy kinetic energy
GmMmv
rSolve for r
Not even light can escape (v=c) if it is closer than r to a black hole. This is the Schwarzschild radius:
R(for v=c) =_____________________
![Page 8: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/8.jpg)
Lab
height and speed vs time
0.00
5.00
10.00
15.00
20.00
25.00
0 0.5 1 1.5 2 2.5
time(s)
height(m)
speed(m/s)
Hand in before lab:• Excel practice results• Pre-lab
Lab this afternoon• Read lab guidelines• Take notes in a bound
notebook• Write up report this
weekend
Kinetic and Potential energy vs time
0
10
20
30
40
50
60
70
0 0.5 1 1.5 2 2.5
time(s)
Kinetic(J)
Potential(m/s)
![Page 9: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/9.jpg)
Astro-B: C&O Ch.2: Gravity & orbits
2 2 34GMT R
Kepler’s laws (for M>>m) Generalization (for M~m)
K1: orbits are elliptical - about center of mass
K2: equal areas in equal times - conservation of L
K3:
Center of mass
Virial Theorem
2 2 34G M m P a
![Page 10: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/10.jpg)
Center of Mass reference frame
Total mass = M = m1+ m2
Reduced mass =
Total angular momentum L=r v = rp vp
1 2
1 2
mm
m m
21L GMa e (Pick any point, e.g. perihelion: rp and vp) p.50
![Page 11: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/11.jpg)
Virial Theorem <E> = <U>/2
where <f> = average value of f over one period
For gravitationally bound systems in equilibrium, the total energy is always one-half of the potential energy.
Ex: Use K3 in Eorbit = T + U for circular orbit:
New HW: 2.8, 2.9
![Page 12: Physics of Astronomy Winter Week 6 - Thus.16.Feb.2006 Astro-A: Universe 4 – Gravity and Orbits Pre-lab – brief discussion Astro-B: Finish C&O Ch.2 2:30.](https://reader036.fdocuments.us/reader036/viewer/2022082821/5697c01b1a28abf838ccf46a/html5/thumbnails/12.jpg)
Looking ahead
Monday Tuesday Wed Thus Fri