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Moisture Resistant Primer for Composite Bonded Repairs

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CB18P
Agency Tracking Number: 075078
Amount: $100,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A1.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-01-18
Award End Date (Contract End Date): 2008-07-21
Small Business Information
9621 Camino Del Sol NE
Albuquerque, NM 87111-1522
United States
DUNS: 859106296
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Andrea Hoyt Haight
 Principal Investigator
 (505) 346-1685
 adherent@earthlink.net
Business Contact
 Susan Switzer
Title: Business Official
Phone: (505) 346-1685
Email: adherenttech@comcast.net
Research Institution
N/A
Abstract

Aging and durability of aircraft in both the military and civilian sectors are becoming major issues as the existing fleet continues to age. Additionally, the increased use of composite structures in the civilian fleet, such as in the Boeing 787 Dreamliner and the Airbus A380, make the understanding and/or improvement of composite durability, particularly durability of repairs, even more critical. Several areas have been identified as targets for improvement in composite aircraft repair. These include the development of rapid, low temperature repair methods and associated materials as well as development of the quality of repairs when they are made. Adhesion of bonded repairs is one area that needs to be addressed.
Adherent Technologies, Inc. is proposing a novel moisture-resistant primer system for use in repairs of standard carbon/epoxy composites used in many subsonic aircraft. Our proprietary chemistry comprised of a reactive coupling agent and a carrier resin compatible with standard aerospace epoxy resins bonds directly to the prepared aircraft composite surface while retaining residual functionality that can be cured directly into the matrix of the repair leading to a covalently bound repair, thereby strengthening the repair interface. Proper selection of the coupling agent structure and carrier resin can serve to further enhance the moisture resistance and thereby durability of the composite repair.

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

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