nico, schmedemann department of earth sciences, institute of geological sciences the age and...
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Nico, SchmedemannDepartment of Earth Sciences, Institute of Geological Sciences
The Age and Cratering History of Phobos
Comparison of two Endmember Chronologies
2The Age and Cratering History of Phobos, Sept 21 2015
OutlineBackground:
• dating of planetary surfaces from measurements of crater size-frequency distributions• the crater production function
• calibration of the lunar chronology function
• scaling the lunar crater production/chronology functions to Phobos
Phobos measurements:
Deimos Quick Look
Conclusions
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Background
Dating of Planetary Surfaces from Measurements
of Crater Size-Frequency Distributions (CSFD)
The Age and Cratering History of Phobos, Sept 21 2015
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Dating of Planetary Surfaces from Measurements of Crater Size-Frequency Distributions (CSFD)
Crater size-frequency measurements are a powerful tool of remote-sensing for age estimations on planetary surfaces. It provides the time frame of geological processes on planetary bodies, where radiometric age determination of rock samples is impossible. It also allows for dating vast areas for little cost, while expensive radiometric samples give ages, just from the actual sample site.
Iapetus 951 Gaspra, Deimos, Phobos 4 Vesta
Dawn Cassini Galileo, Mars-Express
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Background
Crater Production Function
The Age and Cratering History of Phobos, Sept 21 2015
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Crater Production Function
Measuring the crater sizes inside geologic units reveals a functional relationship between the crater sizes and the frequency of the crater sizes.
“Crater Size-Frequency Distribution”
Apollo 12 landing site, image: LRO
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Crater Production Function
Measuring the crater sizes inside geologic units reveals a functional relationship between the crater sizes and the frequency of the crater sizes.
“Crater Size-Frequency Distribution”
The measured crater size-frequency distribution can be approximated by the crater production function (solid line figure left)
Neukum and Ivanov (1994)
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Crater Production Function
The production function can be approximated by a polynomial of 11th degree:
gives the relationship between crater frequencies and the respective crater diameters on a planetary surface
It is stable since at least 3.5 Ga. (Is matter of discussion for earlier times.)
The wavy characteristics is due to the collisional evolution of the main projectile source (Main Belt Asteroids).
+a2(log(D))2+…+a11(log(D))11
Neukum and Ivanov (1994)
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Crater Production Function
1 Ga
4 GaWith increasing exposure age of the surface the crater frequency is rising.
vertical up-shift of representative crater production function (isochrone)
amount of up-shift is defined by the crater chronology function
On the Moon the 4 Ga isochrone plots abouta factor of 100 above the 1 Ga isochrone.
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Crater Production Function
Pitfall “Equilibrium”
• For continued exposure of already densely cratered surfaces the production function turns into an equilibrium distribution.
• Where the slope of the production function is steeper than -3 it will turn into a shallower slope of about -2.
𝑁𝑒𝑞𝑢=10𝑘D−2 (e.g. Neukum & Ivanov, 1994)
Nequ : equilibrium crater frequency k : =1.1 on lunar highlands, but similar on other bodies too D : crater diameter
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Crater Production Function
Pitfall “Resurfacing-Kink”
• Measured crater distributions show kinks if geologic processes erased smaller craters that formed before the process stopped. Larger unaffected craters show higher exposure ages than smaller craters which formed after the resurfacing event.
A step-like structure is usually an indicator for resurfacing. Small craters formed after the erosion event.
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Crater Production Function
Pitfall “Secondary Craters”
• Measured crater distributions can also show distributions steeper than the production function if the measured area is contaminated with secondary craters. In many cases secondary craters can be identified by their clustering.
Excess of small craters possibly from secondaries or image artefacts.
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Crater Production Function
Relative stratigraphic relationships of different surface units of the same planetary body can be identified by measuring the crater size-frequency distribution and fitting the crater production function.
Crater frequencies can be compared at very different crater diameters.
older
younger
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Background
Calibration of the Lunar Chronology Function
The Age and Cratering History of Phobos, Sept 21 2015
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Calibration of the Lunar Chronology Function
young areas = few craters
Relative Ages:
old areas = many craters
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Calibration of the Lunar Chronology Function
A17A15
A14A12
L24
A16
L20
L16
rock/soil ages at sample sites
collecting lunar rock/soil samples
radiometric age dating
A11
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Calibration of the Lunar Chronology Function
• The distribution of radiometric ages derived from lunar rock samples and the measured crater frequencies inside the sampled geologic units give anchor points for the lunar chronology function.
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Calibration of the Lunar Chronology Function
• Prominent peaks around 3.9 Ga of lunar highland samples led to the conclusion of a terminal lunar cataclysm in which most of the lunar basins were formed.
LHB
?
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Calibration of the Lunar Chronology Function
• But: Rock samples were collected exclusively from the top lunar surface. If a late basin (Imbrium) covered all sample sites with thick ejecta blankets, the samples predominantly date the Imbrium impact event.
• older less prominent peaks may point to pre-Imbrium impact events such as Serenitatis (Apollo 17)
• 40 years of discussion
LHB
?
Image from:http://www.psrd.hawaii.edu/Aug06/cataclysmDynamics.html
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Calibration of the Lunar Chronology Function
Neukum and Ivanov (1994)
The non-cataclysm lunar crater chronology by Neukum:
• One of several possible fits through given data points.
• Exponential decay is in agreement with dynamical models based on the cataclysm/LHB view for ages ≤4.1 Ga.
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Calibration of the Lunar Chronology Function
Lunar Chronology after Neukum and Ivanov (1994)
t – surface age in Ga
The chronology function convert crater frequencies into absolute model ages
𝑁 (1 )=5.44∗10−14¿
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Relationship between production function and chronology function:
• Vertical axes of both plots are identical
• Measured cumulative crater frequency at 1 km diameter is converted into an absolute age by the chronology function.
Calibration of the Lunar Chronology Function
1 Ga
4 Ga
Lunar Crater Production Function
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Background
Scaling the Lunar Crater Production/Chronology Functions to Phobos
The Age and Cratering History of Phobos, Sept 21 2015
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Scaling the Lunar Crater Production/Chronology Functions to Phobos
Problems:
• Impact conditions on Phobos are a lot different from the Moon
• Is Phobos a captured asteroid? Chronology of a Main Belt asteroid?
• Phobos’ current orbit is not stable. What was the dynamical situation of Phobos when most of its visible craters were formed.
Solution Part 1:
• Ivanov (2001) scaled the lunar crater production function and lunar chronology to the impact conditions of Mars. The same projectile population was assumed.
Solution Part 2:
• Use of the framework by Ivanov (2001) to derive the crater production function for Phobos for two Endmember cases of its dynamical evolution.
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Scaling the Lunar Crater Production Function to Phobos
Endmember Cases:
A. Phobos has ever been a satellite of Mars in its current orbit
o Average projectile impact velocities are converted form Mars to Phobos’ orbit
o Average impact rate equals Martian impact rate – corrected for different crater scaling
B. Phobos is a recently captured asteroid and nearly all of its craters formed inside the asteroid Main Belt.
o Average projectile impact velocities equals average Main Belt impact velocities
o Average impact rate equals average Main Belt impact rates
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Scaling the Lunar Crater Production Function to Phobos
𝐷𝑡
𝐷𝑃( 𝛿𝜌 )0.43
(𝑣𝑠𝑖𝑛𝛼)0.55
= 1.21[ (𝐷𝑠𝑔+𝐷𝑡 )𝑔 ]0.28
Ivanov (2001; corrected exponents by Ivanov (2008))
= D
If D < Dsimple to complex transition then Dt ~ D
If D > Dsimple to complex transition then
D – observed crater diameterDt – transient crater diameterDP – impactor diameterG – gravity acceleration of target bodyδ – projectile density ρ – target densityv – impact velocityα – impact angleDsg – strength to gravity transition crater diameter
(Dt>>Dsg -> gravity regime; Dt<<Dsg -> stregth regime)
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Scaling the Lunar Crater Production Function to Phobos
Moon Phobos (Case A)Phobos Asteroid Case (Case B)
Target Density (g/cm³)2.5
(est. surface regolith)
1.9(Willner et al.,
2010)
1.9(Willner et al.,
2010)
Projectile Density (g/cm³) 2.5 2.5 2.5
Impact Velocity (km/s) 17.5 8.5 5.3
Impact Angle (most probable case after Gilbert, 1893)
45 4545
Surface Gravity (m/s²) 1.626x10-3
(Willner et al., 2010)
6x10-3
(Willner et al., 2010)
Diameter Strength to Gravity Transition (km)
0.3 81 81
Diameter Simple to Complex (km) 15 4053 4053
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Scaling the Lunar Crater Production Function to Phobos
The Age and Cratering History of Phobos, 21 SEP 2015
Resulting production and chronology functions for cases A and B
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“Nico-Question” from last seminar
The Age and Cratering History of Phobos, 21 SEP 2015
On Phobos (Case A) a crater of 0.5/1/10 km diameter is forming once in ~ 0.1/0.8/4.1 Ga.
What is the age of the youngest crater? Small craters form much more frequent than large craters.
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Phobos Measurements
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Phobos Measurements
HRSC Basemap: Wählisch et al. (2010)
Shown data is publisched in Schmedemann et al, 2014 (doi:10.1016/j.pss.2014.04.009)
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Phobos Measurements
Average Surface to the West of Stickney: N-S grooves stratigraphically above E-W grooves
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Phobos Measurements
Cumulative crater plots of average area west of StickneyAge of Phobos equals last global resurfacing event (break-up of parent body)
Min. Age of Phobos
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Phobos Measurements
Area S1: Interior of Stickney
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Phobos Measurements
Cumulative crater plots of S1 area inside Stickney
Age of Stickney
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Phobos Measurements
Area S2: SRC image of Interior of Stickney; N-S grooves stratigraphically below solitary E-W groove
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Phobos Measurements
Cumulative crater plots of S2 area inside Stickney
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Phobos Measurements Randomness Test
Analysis according to Michael et al. (2012)
The spatial distribution of craters within each measured bin is consistent with being random, if the analysis results are between -3 and 3 standard deviations.
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Phobos Measurements
Comparison of cumulative crater plots of average and S1 area.Stratigraphic relations suggest a formation age of grooves ~3.8 Ga/ Stickney ~4.1 Ga.
Min. Phobosformation
Age of groove formation
Age of Stickney/Limtoc
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Deimos Quick Look
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Deimos Quick Look
The Age and Cratering History of Phobos, 21 SEP 2015
Mosaic:http://sbn.psi.edu/pds/asteroid/MULTI_SA_MULTI_6_STOOKEMAPS_V2_0/document/m2deimos/deimos_cyl_viking_mro.jpgTopographic Data: http://sbn.psi.edu/pds/asteroid/EAR_A_5_DDR_SHAPE_MODELS_V2_1/data/m2deimos.tab
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Deimos Quick Look
The Age and Cratering History of Phobos, 21 SEP 2015
Cumulative crater plot for areas 1 and 2. Differential crater plot for areas 1 and 2.
Minimum Age forDeimos
ProbableResurfacing
Possible Resurfacing/Image Issues
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Conclusions
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Conclusion Phobos
• Production and chronology function were derived for two end-member cases of Phobos’ evolution
- Case A: Phobos was always in its current orbit- Case B: Phobos is a recently captured MB asteroid
• Case A is more realistic because it also covers a capture of Phobos in the early Solar System, when a lot more bodies were available for capturing than today.
• Oldest surface age 4.3 Ga last global resurfacing/break-up of Phobos parent
• Age of Stickney: 4 - 4.2 Ga
• Surface ages show multiple resurfacing events, probably connected to the formation of Stickney and the grooves
• Groove formation appears to be ancient (3 – 4 Ga)
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Conclusion Deimos
• Production and chronology functions were derived for the case that Deimos was always in its current orbit (similar to Case A for Phobos)
• Image data is highly inhomogeneous crater distributions are highly distorted on a global scale
• Oldest surface age 3.7/3.8 Ga Minimum for last global resurfacing/break-up of Deimos parent
• Age of region with highest image resolution: 700/800 Ma probable large resurfacing event• A possible resurfacing ~ 40 Ma could also be caused by issues with image quality.
• Much more work and better imaging data is required for better results.
• Many small craters show elongated morphology projection distortion/secondary craters• If they are secondaries/sesquinaries, an external source (Phobos/Mars?) would be required due to
low escape velocity.
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Discussion
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Apex-/Antapex Asymmetry
• Form recent orbit a factor 4 is expected according to Morota et al. (2008).
• Large (old) craters show apex-/antapex ratio of <1 Phobos may have turned over after some larger impact.
• Sparse statistics for large craters inconclusive
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Crater Production Function• Lunar production function is used as base line, because the main
impactor source is the same on the Moon, Phobos and Main Belt asteroids
• Case A
- vimpM = 9.4 km/s (Ivanov, 2008)- vescM = 5 km/s- vescP = 3 km/s- vimpP = 8.5 km/s
• Case B- Average impact velocities among
Main Belt asteroids are calculated following (Bottke et al., 1994)
- vimpP ~=5.3 km/s
Velocity distribution of 682 Main Belt asteroidsD>50 km
Bottke et al. (1994)The Age and Cratering History of Phobos, 21 SEP 2015
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Chronology Function
• Case A- Impact probability of Mars
(Ivanov, 2001) 0.45 x lunar impact rate
- Correction for different crater scaling between Mars and Phobos 0.97 x lunar impact rate (same projectile is forming larger craters on Phobos than on Mars or the same crater size is achieved by smaller projectiles on Phobos)
• Lunar chronology is used as base line, because the main impactor source is the same on the Moon, Phobos and Main Belt asteroids
The Age and Cratering History of Phobos, 21 SEP 2015
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Chronology Function
• Lunar chronology is used as base line, because the main impactor source is the same on the Moon, Phobos and Main Belt asteroids
• Case A- Impact rate at Mars (Ivanov, 2001) 0.45 x
lunar impact rate
- Correction for different crater scaling between Mars and Phobos 0.97 x lunar impact rate (same projectile is forming larger craters on Phobos than on Mars or the same crater size is achieved by smaller projectiles on Phobos)
1 Ga isochrones for Phobos and Mars
1 GaIsochrones
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Chronology Function
• Lunar chronology is used as base line, because the main impactor source is the same on the Moon, Phobos and Main Belt asteroids
• Case B- Average impact probabilities among Main Belt Asteroids are calculated
following (Bottke et al., 1994) Pi ~ 2.9*10-18 km-2/a 2.9*10-9 km-2/Ga - Conversion from intrinsic impact probability to chronology:
f=Pinir2mean (O’Brien and Greenberg, 2005)
f: impact frequency forming craters ≥ 1 km/GaPi: intrinsic impact probabilityni: number of projectiles forming craters ≥ 1 km
o observed number of Main Belt asteroids ≥ 10 km (obs. limit): 9554o crater size on Phobos as average Main Belt asteroid from 10 km projectiles: 104.5 kmo correction factor for frequency of 104.5 km craters to 1 km craters based on Phobos
production function as MBA: 4*103
o ni: 3.8*107
r: mean radius of target body scaled to unit area = (11 km)²/4π*(11 km)²- f ~ 9*10-3
- (Neukum, 1983)The Age and Cratering History of Phobos, 21 SEP 2015
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Topographic Correction
The Age and Cratering History of Phobos, 21 SEP 2015
True shape (blue) of Phobos along its most variable meridian. Topographic deviations from the reference body may lead to significant errors in spatial measurements that are always conducted on the reference body.
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Topographic Correction
The Age and Cratering History of Phobos, 21 SEP 2015
True shape (blue) of Deimos along its most variable meridian. Topographic deviations from the reference body may lead to significant errors in spatial measurements that are always conducted on the reference body.
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Topographic Correction
The Age and Cratering History of Phobos, 21 SEP 2015
Correction between reference and true body surfaces: Inlays: True body cross‐sections along thetopographically most variable meridian for Gaspra, Ida, Lutetia and Vesta are given as blue outlines.Respective reference spheres are indicated as red outlines with the same center as the true‐body crosssections.Main Panel: Minimum and maximum radii for each of the four asteroids are given as ratio withrespect to the radii of the reference spheres along the x‐axis. The y‐axis gives the correction factor for cratersizes (blue) and areas (red) with respect to the ratios indicated along the x‐axis. Vesta as largest body showsthe smallest diversions (<20%) from the spherical reference body. Diversions for Lutetia, the second largestbody in this selection are up to ~40%. Gaspra’s reference sphere diverts up to ~80% from the true bodysurface. Ida’s highly irregular shape diverts up to a factor of about ~2 from its reference sphere. This extremedifference results in a factor of two incorrect crater sizes and a factor of ~4 incorrect areas.