Evaluation of a hypervelocity impact simulation method for orbital debris shield design

Evaluation of a hypervelocity impact simulation method for orbital debris shield design
Author :
Publisher :
Total Pages : 296
Release :
ISBN-10 : OCLC:33943203
ISBN-13 :
Rating : 4/5 ( Downloads)
DOWNLOAD EBOOK
Book Synopsis Evaluation of a hypervelocity impact simulation method for orbital debris shield design by : Justin Hamilton Kerr

Download or read book Evaluation of a hypervelocity impact simulation method for orbital debris shield design written by Justin Hamilton Kerr and published by . This book was released on 1995 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Evaluation of a hypervelocity impact simulation method for orbital debris shield design Related Books

Evaluation of a hypervelocity impact simulation method for orbital debris shield design
Language: en
Pages: 296

Evaluation of a hypervelocity impact simulation method for orbital debris shield design

Authors: Justin Hamilton Kerr
Categories:
Type: BOOK - Published: 1995 - Publisher:

DOWNLOAD EBOOK

Design of Orbital Debris Shields for Oblique Hypervelocity Impact
Language: en
Pages: 112

Design of Orbital Debris Shields for Oblique Hypervelocity Impact

Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-17 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

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 sp
Hypervelocity Impact Analysis of International Space Station Whipple and Enhanced Stuffed Whipple Shields
Language: en
Pages: 299

Hypervelocity Impact Analysis of International Space Station Whipple and Enhanced Stuffed Whipple Shields

Authors: Michael E. Kalinski
Categories:
Type: BOOK - Published: 2004-12 - Publisher:

DOWNLOAD EBOOK

The International Space Station (ISS) must be able to withstand the hypervelocity impacts of micrometeoroids and orbital debris that strike its many surfaces. I
Numerical Simulation of Ballistic Limit Curves for Orbital Debris Shielding
Language: en
Pages: 0

Numerical Simulation of Ballistic Limit Curves for Orbital Debris Shielding

Authors: Robert James Rabb
Categories:
Type: BOOK - Published: 1998 - Publisher:

DOWNLOAD EBOOK

EXOS is a recently developed particle finite element code well suited to modeling hypervelocity impact phenomena. A series of EXOS simulations were conducted to
Particle Hydrodynamics with Material Strength for Multi-Layer Orbital Debris Shield Design
Language: en
Pages: 42

Particle Hydrodynamics with Material Strength for Multi-Layer Orbital Debris Shield Design

Authors: National Aeronautics and Space Adm Nasa
Categories: Science
Type: BOOK - Published: 2018-09-16 - Publisher: Independently Published

DOWNLOAD EBOOK

Three dimensional simulation of oblique hypervelocity impact on orbital debris shielding places extreme demands on computer resources. Research to date has show