Effects of mass transfer between Martian satellites on surface geology

Abstract

Impacts on planetary bodies can lead to both prompt secondary craters and projectiles that reimpact the target body or nearby companions after an extended period, producing so-called sesquinary craters. Here we examine sesquinary cratering on the moons of Mars. We model the impact that formed Voltaire, the largest crater on the surface of Deimos, and explore the orbital evolution of resulting high-velocity ejecta across 500 years using four-body physics and particle tracking.The bulk of mass transfer to Phobos occurs in the first 102 years after impact, while reaccretion of ejectato Deimos is predicted to continue out to a 104 year timescale (cf. Soter, S. [1971]. Studies of theTerrestrial Planets. Cornell University). Relative orbital geometry between Phobos and Deimos plays asignificant role; depending on the relative true longitude, mass transfer between the moons can change by a factor of five. Of the ejecta with a velocity range capable of reaching Phobos, 2542% by mass reaccretes to Deimos and 1221% impacts Phobos. Ejecta mass transferred to Mars is <10%.We find that the characteristic impact velocity of sesquinaries on Deimos is an order of magnitude smaller than those of background (heliocentric) hypervelocity impactors and will likely result in different crater morphologies. The time-averaged flux of Deimos material to Phobos can be as high as 11% of the background (heliocentric) direct-to-Phobos impactor flux. This relatively minor contribution suggests that spectrally red terrain on Phobos (Murchie, S., Erard, S. [1996]. Icarus 123, 6386) is not caused by Deimos material. However the high-velocity ejecta mass reaccreted to Deimos from a Voltaire-sized impact is comparable to the expected back ground mass accumulated on Deimos between Voltaire-sizeevents. Considering that the high-velocity ejecta contains only 0.5% of the total mass sent into orbit, sesquinary ejecta from a Voltaire-sized impact could feasibly resurface large parts of the Moon,

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Document Details

Document Type
Technical Report
Publication Date
Dec 21, 2015
Accession Number
AD1034496

Entities

People

  • Bogdan Udrea
  • Francis Nimmo
  • Michael Nayak

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Coordinate Systems
  • Escape Velocity
  • Flight Paths
  • Geology
  • Geometry
  • Longitude
  • Mass Transfer
  • Materials
  • Mechanics
  • Planetary Sciences
  • Planets
  • Solar Radiation
  • Solar System
  • Three Dimensional
  • Trajectories
  • United States

Readers

  • Astronomy/Astrophysics
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Space
  • Space - Orbital Debris