作者: N.N. Smirnov , K.A. Kondratyev
DOI: 10.1016/J.ACTAASTRO.2009.04.003
关键词: Debris 、 Spacecraft 、 Hypervelocity 、 Radius 、 Space debris 、 Geocentric orbit 、 Materials science 、 Astrobiology 、 Impact crater 、 Mechanics 、 Work (thermodynamics)
摘要: Abstract The aim of this work is to develop simplified model space debris particle collision on solid structures, which would provide closed form solution formulas for determining crater depth, radius and ejected mass being functions impactor mass, speed material both target. will be verified with results experiments.