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Hypervelocity impact response of aluminum multi-wall structuresThe results of an investigation in which the perforation resistance of aluminum multiwall structures is analyzed under a variety of hypervelocity impact loading conditions are presented. A comparative analysis of the impact damage in structural systems with two or more bumpers and the damage in single-bumper systems of similar weight is performed to determine the advantages and disadvantages of employing more than one bumper in structural wall systems for long-duration spacecraft. A significant increase in protection against perforation by hypervelocity projectiles can be achieved if a single bumper is replaced by two bumpers of similar weight while the total wall spacing is kept constant. It is found that increasing the number of bumpers beyond two while keeping the total stand-off distance constant does not result in a substantial increase in protection over that offered by two bumpers of similar weight.
Document ID
19910065702
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schonberg, William P.
(Alabama, University Huntsville, United States)
Bean, Alan J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1991
Publication Information
Publication: Acta Astronautica
Volume: 25
ISSN: 0094-5765
Subject Category
Structural Mechanics
Accession Number
91A50325
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Other

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