Transcript Slide 1

On the determination of the
probability of collisons of NEAS
with the planets
MACE 2006
Rudolf Dvorak
ADG, Institute of Astronomy
University of Vienna
Asteroids (Minor Planets)
are present everywhere in
our Solar System
Orbital elements of mercury
Eccentricity of Venus and Earth
Mercury
Venus
Earth
Mars
Jupiter
number of asteroids
200
N
u
m
b150
e
r
o
f
A100
s
t
e
r 50
o
i
d
s
3:1 8:3
5:2
2:1
1:1
4:1
Hungarias
Trojans
NEAs
3:2
Hildas
ATENs APOLLOs AMORs
0
1
2
3
semimajor axis [AU]
Semimajor axis AU
4
5
TWO MAIN QUESTIONS
• Transport of Asteroids to become NEAs
• Fading of the NEAs
Transport from the mainbelt connected to the removal
because of the resonances caused by Jupiter
‚Fading‘ caused by collisions with
terrestrial planets, by close encounter
and ejections and by falling into the sun
• O‘Brien and Greenberg, Icarus 178 (2005)
• The collisional and dynamical evolution of the mainbelt and NEA size distribution
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Collisions in the main-belt (Öpik, 1951)
Mean Motion Resonances (MMR)
Yarkovsky effect (radiation force on asteroids)
Resonance escape routes (overlapping of MMR)
Secular resonances
Resonant escape routes  NEAs
• The removal from resonances is caused by CHAOS!
An asteroid in a resonances (Mean motion resonance MMR
suffers from larger perturbations from Jupiter than outside a
resonance. The acting of small divisors because of the MMR
causes large perturbations and shift the asteroid to larger and
larger eccentricities (still smaller than 0.1).
Then a sudden (thousands of years) increase in eccentricities
up to 0.3 and 0.4 leads to a region where the so called
OVERLAPPING of resonances is acting.
This causes eventually an even larger eccentricity with later
encounters to Jupiter (also of Mars).
These encounters lead also to highly chaotic orbits
PHASE SPACE OF THE PENDULUM
x-axis: amplitude; y-axis: velocity
2 types of motion: inside libration, and outside circulation
none
Development of the
eccentricity of a fictitious
asteroid inside the 3:1
MMR for 1 million years
after J.Wisdom (1983)
The eccentricity of the asteroid is
proportional to the distance from the centeer
Libration – small ‚circles‘...e  small
Circulation – large ‚banana‘ ... e  large
NEAR EARTH ASTEROIDS
• Asteroids that have orbits that bring them within 1.3 AU
(195 million kilometers) of the Sun are known as Earthapproaching or Near-Earth Asteroids (NEAs).
• NEAs are fragments which came from the main belt by a
combination of asteroid collisions and the gravitational
influence of Jupiter.
• NEAs are grouped into three categories, named
after 1221 Amor, 1862 Apollo, and 2062 Aten.
• Amors: Asteroids which cross Mars' orbit but do
not quite reach the orbit of Earth. Eros.
• Apollos: Asteroids which cross Earth's orbit with
a period greater than 1 year. Geographos
• Atens: Asteroids which cross Earth's orbit with a
period less than 1 year. Ra-Shalom.
The
dynamical
evolution
of 2062
ATEN for
500000
years
CHAOTIC MOTION
• Billiard: Reflexion on the wall
• For two ‚orbits‘ which deviate for a small angle this
angle doubles after each encounter
• NEAs Reflexion whenever comes close to a planet
Dvorak and Freistetter, Planetary and Space Science:
Dynamical Evolution and collisions of asteroids with the
earth
• 1000 fictitious NEAs were investigated in a long term
integrations
• Dynamical model: Venus to Saturn
• Grid of initial conditions in
• Semimajor axes 0.7 < a < 1.45
• Eccentricity 0.1 < e < 0.8
• RESULTS :
• 1. Flow between these groups
• 2. collision probabilities
Dynamical evolution of a fictious Aten for 500000 years
Collisions per 1 billion years:
Subatens
46
Atens
83
Apollos
52
Amors
3
Conclusions
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Collision probabilities:
ATEN every 500 million years
APOLLO every every 200 million years
Consequences: NEAs should disappear
within some 10 million years BUT
• Because of a flux from the main belt
and outer parts a steady state of the
NEA population is postulated
(Wetherhill, Greenberg, O‘Brien...)