Origins of Regular and Irregular Satellites

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Origins of Regular and

Irregular Satellites

ASTR5830

March 21, 2013

12:30-1:45 pm

Regular vs. Irregular Satellites

Regular:

• Coplanar, low eccentricity and small inclination orbits.

• Typically, larger.

• Thought to have formed in situ.

• Inhabit a small fraction of host planet’s Hill sphere.

Irregular:

• Exist in a large range of e and i .

• Typically, smaller.

• Thought to be captured from heliocentric orbit.

• Orbits extend to ~ 0.5 r

H

.

Observational Constraints on Irregular

Satellite Origins

• Large orbital radii: a ~ 0.5r

H

• Large eccentricities: ( 0.1 ~ e ~ 0.7

)

• Large inclinations: i up to 180˚

– Yet, none are found 60˚ < i

< 120˚

Many have retrograde orbits!

• 100’s known to exist (numerically dominant).

Generally smaller than Regular satellites.

Exist in families with similar dynamics.

Why Study the Capture of

Irregular Satellites?

• Requires dissipative mechanism!

– Tidal dissipation

– Pull-down capture

– Gas-drag capture

– Three-body capture (two flavors)

• No such processes exist in solar system today.

• Must have occurred at an early epoch.

Jewitt and Haghighipour (2007)

Kozai Resonances!

Jewitt and Haghighipour (2007)

Jewitt and Haghighipour (2007)

Jewitt and Haghighipour (2007)

Dynamics and Collisions

• Initial population of irregular satellites was perhaps an order of magnitude larger.

• Collisions can occur that remove, or alter, small bodies.

– Collisions w/ planet.

– Collisions with other satellites ( 10 6 yr ).

– Collisions with interlopers.

– Creation of dynamical families.

• Dynamical instabilities can remove satellites from the system – Kozai Resonances.

– Retrograde satellites are more stable than their prograde counterparts.

Kozai Resonance

• Method of pumping up eccentricities, and reducing the periapses, of orbits by reducing inclinations.

sin

2

P

0.4 csc

2 i

P

 

P max

1

6



1

 

P

 for 39.2

o  i

140.8

o

Capture Mechanisms

• Pull-down

– Sudden increase in Hill radius causes capture.

– Works well for retrograde satellites.

– Requires runaway growth.

• Gas-drag

– Friction with gas in an extended envelope.

– Capture efficiency is a a function of size.

– Also requires sufficient gas.

Three- and N-body Capture

• Does not require circumplanetary gas.

• Two main flavors.

– Interactions with existing satellite(s).

– Wide binary (Kuiper belt) object.

• Density of small objects was much higher at early epochs.

Source Regions

• Yet to be identified!

• Either local or non-local.

• Physical properties of irregular satellites dissimilar to Kuiper belt objects.

• Yet, theories of giant planet formation and migration predict a large amount of objects will be scattered into the inner solar system from a disk of planetesimals exterior to

Neptune.

Triton: a case study

• Largest satellite of Neptune.

– d = 2706 km

– rho = 2.061 g cm -3

– a = 354,800 km = 14.4 R

N

= 0.003 r

– Retrograde orbit: i = 156.8˚

H

Probable Kuiper belt object

• Tidal evolution probably changed Triton’s orbit and evolved its surface.

Capture of Triton

• Tidal capture is unlikely because Triton is too far for tides to act on a short enough timescale.

• Gas-drag capture unlikely because of lack of gas around Neptune.

• N-body capture most likely scenario!

– Disruption of regular satellite system.

– Originally had a binary companion.

Triton vs. Pluto

Triton

• M = 2.14x1022 kg

Pluto

• M = 1.25x1022 kg

• R = 1,353.4 km

• rho = 2,050 kg/m3 • rho = 1,795 kg/m3

• Albedo = 0.76

• R = 1,195 km

• Albedo = 0.5-0.7

http://nssdc.gsfc.nasa.gov/planetary/factsheet/

Agnor and Hamilton (2006)

Schmit and Mitchell

(Unpublished)

Schmit and Mitchell

(Unpublished)

Schmit and Mitchell

(Unpublished)

Overview

• Irregular satellites are most likely captured objects.

• Their source region and capture mechanism have yet to be identified.

• The sizes, colors and total number of irregulars has likely been altered since they were captured.

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