Debris and meteoroid proportions deduced from impact crater residue analysis

Details Debris and meteoroid proportions deduced from impact crater residue analysis Debris and meteoroid proportions deduced from impact crater residue analysis

Feb 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995ldef.symp..431b&link_type=abstract

In NASA. Langley Research Center, LDEF: 69 Months in Space. Third Post-Retrieval Symposium, Part 1 p 431-444 (SEE N95-23796 07-9

Computer Science

Earth Orbital Environments, Environment Simulation, Impact Tests, Long Duration Exposure Facility, Meteorite Collisions, Projectile Cratering, Residues, Space Debris, X Ray Analysis, Hypervelocity Impact, Interplanetary Dust, Light Gas Guns, Low Earth Orbits, Micrometeoroids, Mir Space Station, Spaceborne Experiments, Spacecraft Structures, X Ray Spectroscopy

Scientific paper

This study is a further investigation of space-exposed samples recovered from the LDEF satellite and the Franco-Russian 'Aragatz' dust collection experiment on the Mir Space Station. Impact craters with diameters ranging from 1 to 900 micron were found on the retrieved samples. Elemental analysis of residues found in the impact craters was carried out using Energy Dispersive X-ray spectrometry (EDX). The analyses show evidence of micrometeoroid and orbital debris origins for the impacts. The proportions of these two components vary according to particle size and experimental position with respect to the leading edge of the spacecraft. On the LDEF leading edge 17 percent of the impacts were apparently caused by micrometeoroids and 11 percent by debris; on the LDEF trailing edge 23 percent of the impacts are apparently caused by micrometeoroids and 4 percent consist of debris particles - mostly larger than 3 micron in diameter - in elliptical orbits around the Earth. For Mir, the analyses indicate that micrometeoroids form 23 percent of impacts and debris 9 percent. However, we note that 60-70 percent of the craters are unidentifiable, so the definitive proportions of natural v. man-made particles are yet to be determined. Experiments carried out using a light gas gun to accelerate glass spheres and fragments demonstrate the influence of particle shape on crater morphology. The experiments also show that it is more difficult to analyze the residues produced by an irregular fragment than those produced by a spherical projectile. If the particle is travelling above a certain velocity, it vaporizes upon impact and no residues are left. Simulation experiments carried out with an electrostatic accelerator indicate that this limit is about 14 km/s for Fe particles impacting Al targets. This chemical analysis cut-off may bias interpretations of the relative populations of meteoroid and orbital debris. Oblique impacts and multiple foil detectors provide a higher likelihood of detection of residues as the velocities involved are lower.

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