NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High-Strain-Rate Compression Testing of IceIn the present study a modified split Hopkinson pressure bar (SHPB) was employed to study the effect of strain rate on the dynamic material response of ice. Disk-shaped ice specimens with flat, parallel end faces were either provided by Dartmouth College (Hanover, NH) or grown at Case Western Reserve University (Cleveland, OH). The SHPB was adapted to perform tests at high strain rates in the range 60 to 1400/s at test temperatures of -10 and -30 C. Experimental results showed that the strength of ice increases with increasing strain rates and this occurs over a change in strain rate of five orders of magnitude. Under these strain rate conditions the ice microstructure has a slight influence on the strength, but it is much less than the influence it has under quasi-static loading conditions. End constraint and frictional effects do not influence the compression tests like they do at slower strain rates, and therefore the diameter/thickness ratio of the samples is not as critical. The strength of ice at high strain rates was found to increase with decreasing test temperatures. Ice has been identified as a potential source of debris to impact the shuttle; data presented in this report can be used to validate and/or develop material models for ice impact analyses for shuttle Return to Flight efforts.
Document ID
20060008701
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Shazly, Mostafa
(Case Western Reserve Univ. Cleveland, OH, United States)
Prakash, Vikas
(Case Western Reserve Univ. Cleveland, OH, United States)
Lerch, Bradley A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/TM-2006-213966
E-15282
Report Number: NASA/TM-2006-213966
Report Number: E-15282
Funding Number(s)
CONTRACT_GRANT: NNC05VA03P
WBS: WBS 22-376-10-30-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available