AbstractThe aim of this work is to develop simplified model of space debris particle collision on solid structures, which would provide closed form solution formulas for determining crater depth, radius and ejected mass being functions of impactor mass, speed and material of both impactor and target. The model will be verified with results of experiments.
Evaluation of craters formation in hypervelocity impact of debris particles on solid structures
Acta Astronautica ; 65 , 11-12 ; 1796-1803
2009-04-01
8 pages
Article (Journal)
Electronic Resource
English
Debris , Impact , Spacecraft , Hypervelocity , Crater , Earth orbits
Evaluation of craters formation in hypervelocity impact of debris particles on solid structures
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