PowerPoint PresentationSlide 2Slide 3Slide 4Slide 5Slide 6Slide 7Slide 8Slide 9Slide 10Slide 11Slide 12Slide 13Slide 14Slide 15Slide 16Slide 17Slide 18Lunar agglutinateSlide 20Slide 21Slide 22Slide 23Slide 24Slide 25Slide 26PTYS 554Evolution of Planetary SurfacesVacuum ProcessesVacuum ProcessesPYTS 554 – Vacuum Processes2Regolith GenerationRegolith growthTurnover timescalesMass movement on airless surfacesMegaregolithSpace WeatheringImpact gardeningSputteringIon-implantationGaspra – Galileo missionPYTS 554 – Vacuum Processes3All rocky airless bodies covered with regolith (‘rock blanket’)Moon - Helfenstein and Shepard 1999Itokawa – Miyamoto et al. 2007Eros – NEAR spacecraft (12m across)PYTS 554 – Vacuum Processes4Impacts create regolithsPYTS 554 – Vacuum Processes5Geometric saturationHexagonal packing allows craters to fill 90.5% of available area (Pf)In reality, surfaces reach only ~4% of this value NSATArea( )=Pf4pD2=1.15D- 2or log NSAT/ Area( )=- 2log D( )+logPf4pæ è ç ö ø ÷ Log (D)Log (N) NSATArea( )=EfPf4pD2=0.046 D- 2NSATArea( )=ceqD- 2PYTS 554 – Vacuum Processes6Equilibrium saturation:No surface ever reaches the geometrically saturated limit.Saturation sets in long beforehand (typically a few % of the geometric value)Mimas reaches 13% of geometric saturation – an extreme caseCraters below a certain diameter exhibit saturationThis diameter is higher for older terrain – 250m for lunar MariaThis saturation diameter increases with time Deqµ t1b- 2 Ncum=cD- band Nsat=ceqD- 2at D =Deq, N =Nsat, so Deq=cceqæ è ç ö ø ÷ 1 b- 2( )or c =ceqDeqb- 2( )impliesPYTS 554 – Vacuum Processes7Crust of airless bodies suffers many impactsRepeated impacts create a layer of pulverized rockOld craters get filled in by ejecta blankets of new onesRegolith grows when crater breccia lenses coalesceAssume breccia (regolith) thickness of D/4Maximum thickness of regolith is Deq/4 , but not in all locationsSmaller craters are more numerous and have interlocking breccia lenses < Deq/4Shoemaker et al., 1969Growth of RegolithPYTS 554 – Vacuum Processes8Minimum regolith thickness:Figure out the fractional area (fc) covered by craters D→Deq where (D < Deq)Choose some Dmin where you’re sure that every point on the surface has been hit at least once Typical to pick Dmin so that f(Dmin,Deq) = 2hmin of regolith ~ Dmin/4General caseProbability that the regolith has a depth h is: P(h) = f(4h→Deq) / fminMedian regolith depth <h> when: P(<h>) = 0.5Time dependence in heq or rather Deq α time1/(b-2) hmin=heq4 b- 2( )fminpbceq+1é ë ê ù û ú - 1b- 2( )h =heq12heqhminæèçöø÷b- 2+1æèççöø÷÷éëêêùûúú- 1b- 2( )PYTS 554 – Vacuum Processes9Regolith turnoverShoemaker defines as disturbance depth (d) time until f(4d, Deq) =1Things eventually get buried on these bodiesMixing time of regolith depends on depth specifiedCosmic ray exposure ages on Moon10cm in 500 MyrAbout 105 yrs to removePYTS 554 – Vacuum Processes10Regolith modeled as overlapping ejecta blanketsNumber of craters at distance r (smaller than D=2r)Contributes ejecta of thicknessWhere ejecta thickness is:Results (moon, b=3.4)¶T¶t(>r) =6.8r- 0.66m/ Gyrd r, D( )=aD0.742rDæèçöø÷- 3dT >r( )=- 2pr dr d r, D( )-dNcumdDæèçöø÷02ròdDPYTS 554 – Vacuum Processes11Sharp boundaries between mare and highlands are maintained over GyrLittle lateral mixingE.g. Tsiolkovsky CraterPYTS 554 – Vacuum Processes12What make the lunar landscape look so smooth?PYTS 554 – Vacuum Processes13PhobosPYTS 554 – Vacuum Processes14..and other airless bodiesVestaDeimosPYTS 554 – Vacuum Processes15Transport is slope dependentFor ejecta at 45° on a 30° slopeDownrange ~ 4x uprangeNet effect is diffusive transportDownhillPYTS 554 – Vacuum Processes16Ponding of regolith – seen on ErosRegolith grains <1cm move downslopePonded in depressionsPossibly due to seismic shaking from impactsMiyamoto et al. 2007Robinson et al. 2001PYTS 554 – Vacuum Processes17Mega-regolithFractured bedrock extend down many kilometersActs as an insulating layer and restricts heat flow2-3km thick under lunar highlands and 1km under mariaPYTS 554 – Vacuum Processes18The vacuum environment heavily affects individual grainsImpact gardening – micrometeoritesComminution: (breaking up) particlesAgglutination: grains get welded together by impact glassVaporization of materialHeavy material recondenses on nearby grainsVolatile material enters ‘atmosphere’Solar windEnergetic particles cause sputteringIons can get implantedCosmic raysNuclear effects change isotopes – datingCollectively known as space-weatheringSpectral band-depth isreducedObjects get darker and redder with timeSpace WeatheringPYTS 554 – Vacuum Processes19Lunar agglutinatePYTS 554 – Vacuum Processes20Asteroid surfaces exhibit space weatheringC-types not very muchS-types a lot (still not as much as the Moon)Weathering works faster on some surface compositionsSmaller asteroids (in general) are the result of more recent collisions – less weatheredMaterial around impact craters is also fresherS-type conundrum…S-Type asteroids are the most common asteroidOrdinary chondrites are the most numerous meteoritesParent bodies couldn’t be identified, but…Galileo flyby of S-type asteroids showed surface color has less red patchesNEAR mission Eros showed similar elemental composition to chondrites Ida (and Dactyl) – Galileo missionClark et al., Asteroids IIIClark et al., Asteroids IIIPYTS 554 – Vacuum Processes21Nanophase iron is largely responsibleMicrometeorites and sputtering vaporize target materialHeavy elements (like Fe) recondense onto nearby grainsElectron microscopes show patina a few 10’s of nm thickPatina contains spherules of nanophase FeFe-Si minerals also contribute to reddeninge.g. Fe2Si Hapkeite (after Bruce Hapke)SputteringEjection of particles from impacting ionsSolar-wind particlesH and He nuclei Traveling at 100’s of Km s-1Warped Archimedean spiralImplantation of ions into surface may explain reduced neutron countsClark et al., Asteroids IIIPYTS 554 – Vacuum Processes22New impacts and crater rays darkened over
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