Design of Orbital Debris Shields for Oblique Hypervelocity Impact
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 112 |
Release | : 2018-07-17 |
ISBN-10 | : 1723019178 |
ISBN-13 | : 9781723019173 |
Rating | : 4/5 (78 Downloads) |
Download or read book Design of Orbital Debris Shields for Oblique Hypervelocity Impact written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new impact debris propagation code was written to link CTH simulations of space debris shield perforation to the Lagrangian finite element code DYNA3D, for space structure wall impact simulations. This software (DC3D) simulates debris cloud evolution using a nonlinear elastic-plastic deformable particle dynamics model, and renders computationally tractable the supercomputer simulation of oblique impacts on Whipple shield protected structures. Comparison of three dimensional, oblique impact simulations with experimental data shows good agreement over a range of velocities of interest in the design of orbital debris shielding. Source code developed during this research is provided on the enclosed floppy disk. An abstract based on the work described was submitted to the 1994 Hypervelocity Impact Symposium. Fahrenthold, Eric P. Unspecified Center COMPUTERIZED SIMULATION; HYPERVELOCITY IMPACT; SPACE DEBRIS; SPACECRAFT SHIELDING; ELASTIC DEFORMATION; FINITE ELEMENT METHOD; LAGRANGIAN FUNCTION; PLASTIC DEFORMATION; SPACECRAFT STRUCTURES; SUPERCOMPUTERS...