NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Shield Design For Protection Against Hypervelocity ParticlesInstalling multilayer insulation against primary Whipple bumper reduces pressure-wall damage. Protection to Space Station based on Whipple bumper concept, "Multishock Shields Containing Aluminum Mesh" (MSC-21792). In addition to Whipple bumper, thermal insulation required and provided by multilayered insulation (MLI) consisting of 20 layers (alternating) of double-aluminized Mylar(R) and Dacron(R) netting. When MLI located against bumper, material still disintegrates, but extra space between MLI and pressure wall allows debris pressure cloud to expand so pressure cloud loading reduced. In addition, total amount of MLI material damaged considerably less when placed against Whipple bumper, which contributes to decrease in excess pressure and contents of expanding debris cloud.
Document ID
19930000787
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Schwinghamer, R. J.
(NASA Marshall Space Flight Center, Huntsville, AL.)
Whitaker, A.
(NASA Marshall Space Flight Center, Huntsville, AL.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-28523
Report Number: MFS-28523
ISSN: 0145-319X
Accession Number
93B10787
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available