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Investigating Amorphous Metal Composite Architectures as Spacecraft Shielding

Davidson, Marc and Roberts, Scott and Castro, Gerhard and Dillon, Robert Peter and Kunz, Allison and Kozachkov, Henry and Demetriou, Marios D. and Johnson, William L. and Nutt, Steve and Hofmann, Douglas C. (2013) Investigating Amorphous Metal Composite Architectures as Spacecraft Shielding. Advanced Engineering Materials, 15 (1-2). pp. 27-33. ISSN 1438-1656. https://resolver.caltech.edu/CaltechAUTHORS:20130409-111323153

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Abstract

The threat of micro-meteoroid and orbital debris (MMOD) collisions with spacecraft and satellites has been increasing with the increasing worldwide use of low earth orbit. Providing low-areal-density shielding for the mitigation of these high velocity impacts is essential for ensuring successful and cost effective missions. Here, we report results obtained from hypervelocity impact testing on bulk metallic glass (BMG) matrix composites. Their carbide-like hardness, low melting temperatures, ultra-high strength-to-weight ratio and the ability to be processed like polymers are material attributes ideally suited for spacecraft shielding, particularly as an outer wall bumper shield.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.1002/adem.201200313DOIUNSPECIFIED
http://onlinelibrary.wiley.com/doi/10.1002/adem.201200313/abstractPublisherUNSPECIFIED
Additional Information:© 2013 Wiley-VCH Verlag GmbH & Co. Received: October 11, 2012. Final Version: November 1, 2012. Published online: December 11, 2012. This work was supported by the Strategic University Research Partnership at the Jet Propulsion Laboratory, California Institute of Technology. Graduate student support was provided by the Office of Naval Research under grant no. N00014-07-1-1115, the Education Office of the Jet Propulsion Laboratory, California Institute of Technology, and NASA’s Exploration Systems Mission Directorate under contract number NNH10ZTT001N. The authors thank the staff of the NASA Ames Vertical Gun Range for their technical support of this effort, especially D. Holt and C. Cornelison. The authors also thank Eric Christiansen of NASA’s Johnson Space Center for supplying the ballistic limit equations program and comments.
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Funding AgencyGrant Number
JPL Strategic University Research Partnership ProgramUNSPECIFIED
Office of Naval Research (ONR)N00014-07-1-1115
JPL Education OfficeUNSPECIFIED
CaltechUNSPECIFIED
NASA Exploration Systems Mission DirectorateNNH10ZTT001N
Issue or Number:1-2
Record Number:CaltechAUTHORS:20130409-111323153
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20130409-111323153
Official Citation:Davidson, M., Roberts, S., Castro, G., Dillon, R. P., Kunz, A., Kozachkov, H., Demetriou, M. D., Johnson, W. L., Nutt, S. and Hofmann, D. C. (2013), Investigating Amorphous Metal Composite Architectures as Spacecraft Shielding. Adv. Eng. Mater., 15: 27–33. doi: 10.1002/adem.201200313
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:37826
Collection:CaltechAUTHORS
Deposited By: Ruth Sustaita
Deposited On:09 Apr 2013 18:45
Last Modified:03 Oct 2019 04:51

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