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Autor:
Gennadi V. Belov, Yuri N. Bukharev, Nikolay V. Lapichev, Georgi S. Smirnov, Gennagi V. Bebenin, Yuli A. Fateev, Vadimir I. Zhukov, Vadim V. Bashurov, Georgy P. Schlyapnikov, Anatoli L. Mikhailov, Andrey G. Ioilev
Publikováno v:
International Journal of Impact Engineering. 20:69-78
Results of three sets of experiments modelling space debris impact to spacecraft shield protection in velocities range of 0.5–6.5 km/s are presented. Numerical simulation in the experiments conditions was performed with the help of 3D code KERNEL b