Low-Cost Self-Assembly Technique for a Fully-Integrated Light-Weight Metal Rubber™ Corrosion Sensor System

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-07-C-0275
Agency Tracking Number: N071-038-0510
Amount: $149,998.00
Phase: Phase I
Program: SBIR
Awards Year: 2007
Solicitation Year: 2007
Solicitation Topic Code: N07-038
Solicitation Number: 2007.1
Small Business Information
P.O. Box 618, Christiansburg, VA, 24068
DUNS: 008963758
HUBZone Owned: Y
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 A. Hill
 Director of Program Development
 (540) 953-1785
 ahill@nanosonic.com
Business Contact
 Lisa Lawson
Title: Contracts Administrator
Phone: (540) 953-1785
Email: llawson@nanosonic.com
Research Institution
N/A
Abstract
NanoSonic proposes to develop a durable fully-integrated nanostructured sensor to detect surface-related phenomena, such as wear/corrosion, of military aircraft; specifically, a Metal Rubber(TM) corrosion detection system. Metal Rubber™ (MR™) is a multifunctional nanostructured material that can have high electrical-conductivity, low-modulus, and low mass-density. NanoSonic plans to integrate the non-invasive MR™ sensor system onto aircraft structures to detect chemical modifications and microstructural breakdown from corrosion. The in-situ MR™ corrosion detection system would be fully-integrated onto the aircraft surface as a coating or conformal appliqué for a self-assessing “smart” coating system that would reduce timely visual inspections, thus reducing system maintenance costs and improving the overall safety. NanoSonic has established techniques to control multiple constitutive material properties in coatings and free-standing materials using molecular layer-by-layer ESA processes, by varying the type, size, and structure of incorporated molecules. This low-cost method would be used to fabricate conformal corrosion sensor materials that could be applied on existing structural components as coatings or appliqués. MRTM sensors and interconnect elements may be incorporated into the coating (or appliqué) via patterning to allow for a wire-free, in-situ corrosion detection system. Integrating co-located interconnected RF circuits would allow for remote RF mapping of the aircraft surface structural properties.

* Information listed above is at the time of submission. *

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