Model for predicting micrometeoroid/debris impacts and damage to composite materials.

Details Model for predicting micrometeoroid/debris impacts and damage to composite materials. Model for predicting micrometeoroid/debris impacts and damage to composite materials.

Jul 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993spde.conf..231t&link_type=abstract

First European Conference on Space Debris, Proceedings of the Conference held 5-7 April 1993 in Darmstadt, Germany. Edited by W.

Physics

Micrometeoroids: Space Density

Scientific paper

This report first presents an analysis of the published micrometeoroid/debris impact data observed on the Long Duration Exposure Facility (LDEF) which was in orbit for about 5.75 years. LDEF impact data were obtained as a function of angular location relative to the ram direction. Thus is was possible to develop a nomogram that can be used to estimate the total number of impacts that could be expected on a space structure as a function of time in orbit, angular location relative to ram and exposed surface area based on simple extrapolation/interpolation of the LDEF data.

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