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Giant Impacts During Planet Formation:

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Observations: Median disk lifetime 3 Myr, Jupiter 0-3 MEarth Core (Saturn's 9-22 MEarth) ... Saturn: Impact adds mass - grow core more quickly, remove later ... – PowerPoint PPT presentation

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Title: Giant Impacts During Planet Formation:


1
Giant Impacts During Planet Formation
  • Parallel Tree Code Simulations Using Smooth
    Particle Hydrodynamics

2
Why Giant Impacts?
  • Evidence
  • 98 degree obliquity of Uranus
  • Random element of planetary rotation
  • Moon, Mercury, Pluto-Charon
  • Core Accretion vs. Gas Instability Model
  • Metal abundance vs. planet occurrence rate
  • Mass function of planets

3
Impact Effects
  • Shortening Formation Timescales
  • Observations Median disk lifetime 3 Myr, Jupiter
    0-3 MEarth Core (Saturns 9-22 MEarth)
  • Theory Jupiter needs more than 10 Myr to form
    with 3 MEarth Core (and Saturn takes 10 Myr to
    form with 17.5 MEarth core)
  • Effects of migration

4
Shortening Formation Timescales How?
  • Cut off heating from planetesimal accretion
  • Jupiter Start with large core - rapid growth -
    impact removes core mass directly or through
    mixing
  • Saturn Impact adds mass - grow core more
    quickly, remove later planetesimal heating (9.8
    - 3.3 Myrs)

5
Uranus and Neptune
  • Similar core masses accounted for by core
    accretion model
  • Why similar envelope masses?
  • Why thermal emission differences?

6
Goals
  • Core Mass/Formation Time
  • Uranus and Neptune Envelope Mass, Thermal
    Emission
  • Satellite Formation

7
Method
  • SPH with parallel tree algorithm, self-gravity,
    Runge-Kutta-Fehlberg integrator of 2nd order
  • 262,144 particles
  • Radial cutoff at 1010 cm
  • Tillotson, Saumon-Chabrier, ideal gas EOS
  • Continued for 25,000-35,000 seconds (time to
    impact 7-12 free-fall times)

8
Method Comparisons
  • Korycansky 1990
  • 1-D grid code
  • impact onto Uranus
  • produces obliquity envelope dispersal
  • Slattery 1992
  • SPH, 8,000 particles (1 small particle mass of
    entire Uranian satellite system)
  • Uranus impact - disks up to 0.3 MEarth
  • no gaseous envelope
  • Radiative Transfer
  • no reasonable algorithm available when
    simulations were run
  • simulation time

9
Numerical Tests of Code
  • Mass conservation good (
  • Angular momentum conservation within 1043 gm
    cm2/sec (
  • Energy not conserved well (viscosity effects)

10
Numerical Tests of Code
  • Particle Number
  • Earth vs. Mars pressure/density wave propagates
    at sound speed

11
Results
  • Simulations
  • 6 MEarth impactor, 26 km/sec, 5 silicate ice,
    600 particles
  • Impact angles 0/0, 90/15, inf/24 degrees w/r/t
    core/envelope
  • Jup Model A 30.6 MEarth core 6.24 (5) MEarth
    envelope, dust opacity standard model, 3 (of
    3.1) Myr evolution time
  • Jup Model B 14.6 MEarth core 5.0 (3) MEarth
    envelope, dust opacity 0.02 standard model,
    1.75 (of 2.2) Myr

12
Simulation A1
  • Head-on collision with massive proto-Jupiter
    (Model A)
  • 8 of envelope mass escapes
  • Core and impactor remain

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Simulation A1half
  • Same as A1 but half the particles
  • 8 of envelope mass escapes (same as A1)
  • Core and impactor remain
  • Numerical resolution is sufficient

18
Simulation A2
  • Glancing (90 degree impact angle w/ core)
    collision with massive proto-Jupiter (Model A)
  • 4 of envelope mass escapes
  • Majority of impactor 0.14 MEarth of core
    escapes
  • Additional 0.02 MEarth from core 0.06 from
    impactor likely to mix into envelope

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20
Simulation A3
  • Glancing (24 degree impact angle w/ envelope)
    collision with massive proto-Jupiter (Model A)
  • 2 of envelope mass escapes
  • Impactor escapes, core remains

21
Simulation B1
  • Head-on collision with less massive proto-Jupiter
    (Model B)
  • 32 of envelope mass escapes to orbit or to
    nebula
  • 0.2 MEarth of core escapes, impactor remains
  • Additional 0.16 MEarth from core likely to mix
    into envelope

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23
Simulation B2
  • Glancing collision (90 degree impact angle w/
    core) with less massive proto-Jupiter (Model B)
  • 9 of envelope mass escapes to orbit or to nebula
  • Impactor leaves behind only 0.01 MEarth

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25
Simulation B3
  • Glancing collision (24 degree impact angle w/
    envelope) with less massive proto-Jupiter (Model
    B)
  • 2 of envelope mass escapes
  • Core remains, impactor departs intact

26
Results Summary
27
Results Summary
28
Results Timescale/Core Mass
  • Case A1 Shorten formation time by increasing
    core mass
  • Case A2 Shorten formation time by increasing
    core mass some mass liberated from core, but
    more is added to core from impactor
  • Case A3 Little effect on core mass
  • Case B1 Shorten formation time by increasing
    core mass some mass liberated from core, but
    more is added to core from impactor
  • Case B2 Little effect on core mass
  • Case B3 Little effect on core mass
  • A case with intermediate impact angle between B1
    and B2 is likely to result in more core mass
    being lost
  • Upper bound of 0.3 MEarth on core mass mixed with
    deposited energy through convection

29
Results Uranus/Neptune Similarities
  • Case B1 produces envelope mass similar to
    Uranus/Neptune
  • Case B2 produces core mass similar to U/N and
    envelope mass nearly as small
  • Angular momentum values in reasonable agreement
    between Case B2 and Uranus today

30
Results Uranus/Neptune Thermal Emission
Differences
  • Case B1 - compositional gradient at 89 of
    radius (rhoo 2.7 vs. 0.95 g/cm3)
  • Compositional gradients at 50-60 radius require
    impact at much earlier times

31
Results Satellite Formation, Envelope Enrichment
  • Solid satellite disks not formed in any of the 6
    cases
  • Case B1 results in an upper bound of 0.37 MEarth
    of material mixed into envelope ( up to 0.29
    mixed due to convection)

32
Summary
  • Mass and angular momentum well-conserved, energy
    subject to artificial viscosity errors
  • Simulations well-resolved numerically
  • Simulated giant impacts at 2 evolutionary stages
    with 3 impact angles

33
Summary contd
  • Giant impacts disrupt planetary cores, decreasing
    their mass by as much as 0.66 MEarth (but there
    is a net increase in core mass in all cases due
    to added mass of impactor)
  • Core mass loss decreases as a function of initial
    proto-planetary mass and increases with impact
    angle, up to angle unclear)
  • No case resulted in a net loss of core mass, but
    an impact intermediate between B1 and B2 may do
    so
  • Mass added to core by impactor increases as a
    function of initial proto-planet mass and
    decreases as a function of impact angle
  • Up to 0.16 MEarth of core is accelerated to half
    the escape speed, but has insufficient angular
    momentum to create a disk. Impact angle between
    B1 and B2 will provide more non-radial velocity.

34
Summary contd
  • Giant impacts can leave planet with only 2
    MEarth of envelope, similar to Uranus and Neptune
  • Envelope mass removed goes up with decreasing
    impact angle and decreasing core mass
  • Impacts in our models created compositional
    differences down to 89 of planetary radius
  • No significant disks were generated

35
Future Directions
  • Do simulation similar to Case B2 with slightly
    smaller impact angle
  • Likely to result in greater mass loss
  • Improve formulation of artificial viscosity
  • Suite of simulations to determine likelihood of
    envelope mass decrease to 2 MEarth, and to test
    Canup et al 2001 satellite formulae
  • Impact simulations at earlier times to determine
    likelihood of compositional gradient at 50-60
    radius
  • Use more recent (Hubickyj et al 2005) planet
    models, add migration effects, make choice of
    impactor characteristics more sophisticated, use
    impactors with rock/ice layers

36
Conclusion
  • Giant impacts can affect planetary evolution
  • Thanks to Peter (!), Doug and Steve for their
    support!
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