作者: N.N. Smirnov , A.B. Kiselev , M.N. Smirnova , V.F. Nikitin
DOI: 10.1016/J.ACTAASTRO.2014.09.014
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摘要: Abstract The paper gives coverage of recent advances in mathematical modeling long term orbital debris evolution within the frames continua approach. Under approach equations contain a number source terms responsible for variations quantities different fractions population due to fragmentations and collisions. Mechanisms hypervelocity collisions fragments with pressurized vessels are investigated. spacecraft shield honeycomb concept is suggested based on principles impact energy conversion redistribution consumption by destroyable structures. devoted 100th anniversary founder space research Moscow State University Prof. G.A. Tyulin.