B. A. Ivanov Institute for Dynamics of Geospheres, RAS, 119334, Moscow, Russia, CTX_P05_003145_2050_XI_25N098W HiRISE PSP_6758_2050.

Slides:



Advertisements
Similar presentations
Mars/moon impact rate ratio: 2000/2012 comparison Impact craters as a link to other terrestrial planets, satellites and asteroids Interplanetary comparisons.
Advertisements

Probabilistic Inverse Dynamics for Nonlinear Blood Pattern Reconstruction Benjamin Cecchetto, Wolfgang Heidrich University of British Columbia.
November 12, 2013Computer Vision Lecture 12: Texture 1Signature Another popular method of representing shape is called the signature. In order to compute.
The Radial Variation of Interplanetary Shocks C.T. Russell, H.R. Lai, L.K. Jian, J.G. Luhmann, A. Wennmacher STEREO SWG Lake Winnepesaukee New Hampshire.
Martian Craters with Interior Deposits: Global Survey Results and Wind Model P21D-1875 Kristen A. Bennett 1 and Mark Schmeeckle 2 1 School of Earth and.
Important Physical Factors for Liquid Water Forming at the Martian Surface.
Surface Chronology of Phobos – The Age of Phobos and its Largest Crater Stickney 1 N. Schmedemann 1, G. Michael 1, B. A. Ivanov 2, J. Murray 3 and G. Neukum.
The timing of, duration of, and wind patterns driving sand saltation on Mars are typically poorly constrained. The patterns of aeolian activity within.
SEAT Traverse The Satellite Era Accumulation Traverse (SEAT) collected near-surface firn cores and Ultra High Frequency (UHF) Frequency Modulated.
Which describes a variation of wave frequency ω(t) in a geometric-optic approximation [4]. Here n(ω) is the refractive index of the medium, is the vector.
“Rummaging through Earth’s Attic for Remains of Ancient Life” John C. Armstrong, Llyd E. Wells, Guillermo Gonzalez Icarus 2002, vol. 160 December 9, 2004.
Asteroids & Meteors Lectures will be available at: homework.uoregon.edu/pub/elsa/haydock/
Destructive Effects of Nuclear Weapons
Errors in Viking Lander Atmospheric Profiles Discovered Using MOLA Topography Withers, Lorenz, and Neumann LPSC 2002 Abstract #1294 Abstract’s Abstract:
Observations and models of size distribution of KBOs (summarize several articles) Yeh, Lun-Wen
Identifying Interplanetary Shock Parameters in Heliospheric MHD Simulation Results S. A. Ledvina 1, D. Odstrcil 2 and J. G. Luhmann 1 1.Space Sciences.
METO 621 Lesson 27. Albedo 200 – 400 nm Solar Backscatter Ultraviolet (SBUV) The previous slide shows the albedo of the earth viewed from the nadir.
Hyperspectral Satellite Imaging Planning a Mission Victor Gardner University of Maryland 2007 AIAA Region 1 Mid-Atlantic Student Conference National Institute.
Simulator for the observation of atmospheric entries from orbit A. Bouquet (Student, IRAP) D. Baratoux (IRAP) J. Vaubaillon (IMCCE) D. Mimoun (ISAE) M.
Lunar CRater Observation and Sensing Satellite Project LCROSS Site Selection Workshop Oct , 2006 NASA/ARC, Mountain View, California LCROSS Orbital.
Informational and analytical system of dangerous celestial bodies monitoring, and asteroid and comet hazard counteraction planning Hannover, June 2015.
Hydrologic Statistics
Physics 114: Lecture 15 Probability Tests & Linear Fitting Dale E. Gary NJIT Physics Department.
Jay Melosh Purdue University Planetary Defense Workshop, 8 July 2015 Near-Field Damage from Impacts and Airbursts.
ASTRONOMY 340 FALL October 2007 Class #9. Salient Martian Features  R Mars = 3396 km (R Earth = 6378 km)  Higher surface area to mass ratio 
GEF2200 Stordal - based on Durkee 10/11/2015 Relative sizes of cloud droplets and raindrops; r is the radius in micrometers, n the number per liter of.
Properties of Barred Galaxies in SDSS DR7 - OPEN KIAS SUMMER INSTITUTE - Gwang-Ho Lee, Changbom Park, Myung Gyoon Lee & Yun-Young Choi 0. Abstract We investigate.
EGU General Assembly 2013, 7 – 12 April 2013, Vienna, Austria This study: is pioneer in modeling the upper atmosphere, using space geodetic techniques,
CHARACTER OF FREE WATER (ICE) SPREDING IN THE MARTIAN SURFACE REGOLITH ON THE BASE OF HEND/ODYSSEY DATA. by Kuzmin R.O. 1, I.G. Mitrofanov, M.L. Litvak,
Ultimate Spectrum of Solar/Stellar Cosmic Rays Alexei Struminsky Space Research Institute, Moscow, Russia.
Study Design and Summary Atmospheric boundary layer (ABL) observations were conducted in Sapporo, Japan from April 2005 to July Three-dimensional.
Chapter 4 – Gravity, Projectiles, Satellites
Impact Mechanics and Morphology. Impact Craters Crater: From the Greek krater meaning bowl Drop a rock into some sand (v = a few m/sec) –Physically what.
Last week’s problems a) Mass excess = 1/2πG × Area under curve 1/2πG = × in kgs 2 m -3 Area under curve = -1.8 ×10-6 x 100 m 2 s -2 So Mass.
Surface and Bulk Fluctuations of the Lennard-Jones Clusrers D. I. Zhukhovitskii.
Abstract: A simple representative model of the ionosphere of Mars is fit to the complete set of electron density profiles from the Mars Global Surveyor.
Cratering on Nix and Hydra William Bottke (SwRI).
Goal: to understand waves Objectives: 1)To learn about Oscillations and vibrations 2)To understand the properties of Waves 3)To learn about Transverse.
Asteroids. Asteroid Belt An asteroid is a bit of rock Left over after the Sun and all the planets were formed. Most asteroids in our solar system can.
Meteoroid and debris models and tools in SPENVIS H. Ludwig D. Heynderickx BIRA, Ringlaan 3, B-1180 Brussel, Belgium.
Simulations of radio emission from cosmic ray air showers Tim Huege & Heino Falcke ARENA-Workshop Zeuthen,
Page 1 HEND science after 9 years in space. page 2 HEND/2001 Mars Odyssey HEND ( High Energy Neutron Detector ) was developed in Space Research Institute.
Mars - The Red Planet Image Courtesy of NASA/JPL-Caltech.
Nico, Schmedemann Department of Earth Sciences, Institute of Geological Sciences The Age and Cratering History of Phobos Comparison of two Endmember Chronologies.
Extrasolar planets. Detection methods 1.Pulsar Timing Pulsars are rapidly rotating neutron stars, with extremely regular periods Anomalies in these periods.
David Nesvorny (Southwest Research Institute) David Nesvorny (Southwest Research Institute) Capture of Irregular Satellites during Planetary Encounters.
Study of high energy cosmic rays by different components of back scattered radiation generated in the lunar regolith N. N. Kalmykov 1, A. A. Konstantinov.
Quiz #10 What would really happen to you if you were to fall all the way into the Event Horizon of a black hole? We know the gravity is unbelievably strong.
OBLIQUE IMPACT AND ITS EJECTA – NUMERICAL MODELING Natasha Artemieva and Betty Pierazzo Houston 2003.
- Quick review and discussion of upcoming test - Visualize a scale model of the earth, sun and moon - Use the orbital motion of the moon to understand.
Dynamics of Binary Search Trees under batch insertions and deletions with duplicates ╛ BACKGROUND The complexity of many operations on Binary Search Trees.
Making impact craters from numbers Natalia Artemieva Tucson-2007.
Section 4: Earth’s Moon. What are we learning about today? 1. What features are found on the moon’s surface? 2. What are some characteristics of the moon?
The Moon Itself Structure and Atmosphere. Basic Lunar Stats Radius: 1,738 km ( 26 % of Earth’s) Mass:.0123 Earth Masses (7.349 x 10^22 kg) Density: 3.34.
Cratering in the Solar System William Bottke Southwest Research Institute Boulder, Colorado.
Unit 11 Mars. Physical Properties Radius: 3400 km Moons: Deimos, Phobos Mass: 6.4 × kg Density: 3900 kg/m 3 Length of Day: 24.6 hours.
Integrating LiDAR Intensity and Elevation Data for Terrain Characterization in a Forested Area Cheng Wang and Nancy F. Glenn IEEE GEOSCIENCE AND REMOTE.
8 th February 2006 Freddy Poirier ILC-LET workshop 1 Freddy Poirier DESY ILC-LET Workshop Dispersion Free Steering in the ILC using MERLIN.
Fundamentals of Data Analysis Lecture 10 Correlation and regression.
U.A. Dyudina, A.P. Ingersoll, California Institute of Technology Pasadena, CA, Objectives We study lightning on Jupiter using spatially resolved.
Comets are probably left over from the time when the planets formed.
Crater models and possible scaling law
33 (6 outlines) -> 27.
Lecture 12 The Importance of Accurate Solar Wind Measurements
A.S. Lidvansky, M.N. Khaerdinov, N.S. Khaerdinov
Computer Vision Lecture 16: Texture II
Chapter 27 Early Quantum Theory
Projectile motion can be described by the horizontal and vertical components of motion. Now we extend ideas of linear motion to nonlinear motion—motion.
by Asaf Inbal, Jean Paul Ampuero, and Robert W. Clayton
The Mars Pathfinder Atmospheric Structure Investigation/Meteorology (ASI/MET) Experiment by J. T. Schofield, J. R. Barnes, D. Crisp, R. M. Haberle, S.
Presentation transcript:

B. A. Ivanov Institute for Dynamics of Geospheres, RAS, , Moscow, Russia, CTX_P05_003145_2050_XI_25N098W HiRISE PSP_6758_2050 October MS3-1-3 No No Yes!

 HiRISE resolution from 25 to 30 cm/pixel allows us recognize small craters with D≥ 1.5 m  Main attention is devoted to young small craters with the age of 10 years and younger.  19 of 20 young craters from Malin’s collection (Malin M.C. et al.,2006, Science, 314, ) are confirmed  Now the list of dated (“new”) small craters has more than 140 candidates  Data processing is finished for ~140 cases  About 50% of impacts create clusters of craters October MS3-1-3

Martian atmosphere Atmospheric density at 15 km altitude is the same as at 40 km above the Earth surface. Projectiles making bolides on Earth, are able to record themselves making craters on Mars October MS3-1-3

Welcome the Town of Young Craters!  Location: dusty areas on Mars ( where easy to find )  Population: from 1 to 3000 individual craters in a cluster (clustered and single crater cases are ~50/50)  Altitude: from -6km to +18 km (in respect to the smoothed areoid surface)  Maximum size to date: D~35 m (N D>31.25 =3) October MS3-1-3

Location of new craters October MS3-1-3

Almost all new impact sites found over dusty areas October MS3-1-3

Largest new crater (54m) October MS3-1-3 Smallest new crater (~2.5 m) formed between April 2006 and February 2008 (ESP_016660_1860) Not all craters are as simple …

Atmospheric breakup 0.5 v T Circle: 2 r = v T *t flight Ellipse: 2a = r/sin , 2b=r Z Z/sin  PPT=Plane Perpendicular to Trajectory Passey&Melosh, 1980, Icarus 42 (2), v PSP_09185_1770 Ellipse 137x37 m Apparent angle ~15 o October MS3-1-3

Cluster at lowermost altitude (Hellas): h=-6.36 km (PSP_007596_1295), m 75.59,m D max ~ 5.2 m  m ~3000 kgm -3 Z~ 3 km (+6 km below zero)  10 ~11 bar Minimum altitude: size 7 m, population N>49 October MS3-1-3

New Impact Site Formed between November 2007 and February 2009 (ESP_013707_1915) =42 m, D max ~ 3.2 m Maximum altitude of 18 km: size 5 m, population N>23 October MS3-1-3

Single fragmentation  Shock wave interaction gives small transversal velocity v T to fragments  C T ~ 0.9 (derived from the numerical modeling) corresponds to separation of craters on surface of the order of 30 to 50 m on Mars  Atmospheric density at the fragmentation point defines stagnation pressure at the breakup, proportional to the effective strength   a v 2  The final separation radius in PPT is a function of Z with a maximum at ~22 km on Mars (at v=10 km/s  ~ 2 bar – similar to Earth bolides) 0.5 v T ArtemievaA&Shuvalov, JGR 106, , 2001 October MS3-1-3

Three levels of modeling 1.Geometrical modeling: assumes one craters-one fragment, takes care only about location of craters with a weak role of the fragment (crater) size. Gives quick estimates of break up parameters 2. Analytical solution to fragment deceleration with a constant ablation coefficients (recognizes ice, CC, OC, and iron meteoroids) 3.Direct 3D modeling of each fragment atmospheric passage with the ablation ##2 and 3 needs to assume a scaling law for crater sizes. Currently we use porous (dry sand) scaling with a possibility to have strength-to-gravity transition for D=1 to 10 m. Loose dust? How thick? What is the substrate? Projectile sizes for our crater collection is below ~2 m in diameter October MS3-1-3

Cascade fragmentation October MS3-1-3 ESP_016200_1740 altitude of 5.4 km The first fragmentation event happened at stagnation pressure of 0.32 MPa (3.2 bar), while further fragmentation events occur at 0.42 to 0.49 MPa (4.2 to 4.9 bar).

Cascade model: Each fragment is divided in two subfragments with mass m n = (1-r) m 1 n+1 + r m 2 n+1 ; r is the random number from 0.5 to 1. After N cascade fragmentation events the shower includes 2 N cascade fragments. Largest counted clusters have N cascade from 9 to 13. Cascade model: Size-frequency distribution (SFD) as increment number of craters in diameter bins with diameter step Black – model Color - counted October MS3-1-3

 The most populated claster: >3000 individual craters PSP_003172_1970; formed between 13 December 2004 and 6 May 2006; Deq=36 m, Dmax=17 m Assumed angle of incidence ~30 o Along trajectory Across trajectory Number of craters D>2 per 20-m strips Cascade model Multiple fragmentation enhances crater dispersion in a cluster October MS3-1-3

Other examples: PSP_003259, inclination ~45 o PSP_005375, inclination ~40 o October MS3-1-3

Tentative classification by meteoroid’s density Entry velocity and strength can be estimated as a combination: (  0 – is near-surface atmospheric density) Normalized to a single 2-fragment separation event cluster width (zero for single craters v.s. target surface altitude. Projectiles with the same density and  should follow a straight line started at the disruption altitude (zero separation) Low density (and low ablation!!!) or high c T projectiles??? October MS3-1-3

Searching for the impact rate October MS3-1-3 Cratering rate seems well established for D>15 m as about 3 recognized impact per year

Dating of young areas – Opportunity area October MS3-1-3 Golombek, M., K. Robinson, A. McEwen, N. Bridges, B. Ivanov, L. L. Tornabene, and R. Sullivan (2010), Constraints on ripple migration at Meridiani Planum from Opportunity and HiRISE observations of fresh craters, J. Geophys. Res., doi: /2010JE003628, in press. (accepted 6 August 2010) HiRISE gives orbital view Opportunity gives ground view

Dating of young surfaces October MS3-1-3 Hartmann’s isochrones HiRISE’s isochrones

Size frequency distribution  Observations fit Hartmann’s model in the first approximation (what is amazing!) R a) Estimates for an “effective” single craters b) Integrated model – assumes our collection represent an average cratering style Well cratered surface have a “flat” SFD in R-plot due to overlapped clusters. October MS3-1-3

Conclusions  In contrast to early expectations tiny atmosphere of Mars disrupts ~50% of small projectiles  Some clusters have large dispersion at the surface. Low density (comet)? Higher efficiency of separation (e.g. multiple, not binary fragmentation)?  Complex structure of “apparently fragile” projectiles – weakly bounded aggregates of stronger pebbles? Can they survive long enough in space?  Crater age estimates for D<30 to 50 m should take into account the clustering effect (one entry – hundreds of small craters) October MS3-1-3

Curving albedo patterns due to interaction of atmospheric shock waves generated by near- simultaneous impacts October MS3-1-3