Abstract
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 based on the SPH-method (Smoothed Particles Hydrodynamics) and assigned to obtain prompt solutions of perforation and damage of multilayered and multisheet bumpers under the high- and hypervelocity impact of single particles. Results of numerical simulation are in a good agreement with experimental data.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
