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Wire Insulation Incorporating Self-Healing Polymers (WIISP)

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNK05OA32C
Agency Tracking Number: 040109
Amount: $99,999.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T6.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2004
Award Year: 2005
Award Start Date (Proposal Award Date): 2005-01-21
Award End Date (Contract End Date): 2006-01-23
Small Business Information
2780 Skypark Drive, Suite 400
Torrance, CA 90505-7519
United States
DUNS: 106823607
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Anna Stewart
 Principal Investigator
 () -
 astewart@nextgenaero.com
Business Contact
 Jayanth Kudva
Title: President
Phone: (310) 891-2814
Email: jkudva@nextgenaero.com
Research Institution
 Virginia Tech
 greg reaves
 
460 Turner Street, Mail #0170
Blacksburg, VA 24061
United States

 (540) 231-8217
 Domestic Nonprofit Research Organization
Abstract

NextGen Aeronautics, Inc. and their partner, Virginia Tech, propose to develop a self-healing material for wire insulation using a class of poly(ethylene-co-methacrylic acid) (EMAA) and poly(tetramethylene oxide) ionomer polymers. The self-healing property of these materials is strongly correlated with the thermal processes that occur during and after damage initiation. Recent experimental results have demonstrated that penetration of the polymer by a projectile causes localized heating near the puncture. The heating then causes a localized melt elastic response which serves to close the puncture and 'heal' the polymer.

Since self-healing has already been demonstrated using these materials, the major technical challenge of this STTR effort is to stimulate the localized melt elastic response that has been shown to initiate self-healing. Our concept is to incorporate a magnetically-response phase into the insulating polymer for the purpose of causing localized heating during high-frequency excitation of the polymer. This magnetic phase will be located close to the electrical conductor. Localized heating will cause flow into the crack and, upon cooling, the crack will close over the wire and eliminate the exposure of the bare wire.

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

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