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HybridSil® Advanced, Heat Tolerant Towlines for Aircraft Towed Decoys

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-22-C-0338
Agency Tracking Number: N221-020-0345
Amount: $140,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N221-020
Solicitation Number: 22.1
Timeline
Solicitation Year: 2022
Award Year: 2022
Award Start Date (Proposal Award Date): 2022-07-07
Award End Date (Contract End Date): 2023-01-17
Small Business Information
158 Wheatland Drive
Pembroke, VA 24136-1111
United States
DUNS: 008963758
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Tyler Seguine
 (540) 626-6266
 tseguine@nanosonic.com
Business Contact
 Amanda Moye
Phone: (540) 626-6266
Email: amoye@nanosonic.com
Research Institution
N/A
Abstract

Current towlines for towed aircraft decoys are experiencing catastrophic failures due to the extreme temperatures (> 650 °C) produced from the afterburners during high Angle of Attack (AOA) maneuvers. The hot exhaust leads to towline separation. Additionally, the electrical components within the decoy are susceptible to failure due to the conducting wire insulation breakdown. The goal of this program is to develop a novel polymer derived ceramic (PDC) coating that will act as a thermal protection barrier. NanoSonic shall utilize a combination of our polyorganosiloxanes and polysilazanes, which have proven to survive temperatures >650°C, in combination with ceramic nanoparticles such as aluminum nitride and yttrium silicate. Thermogravimetric analysis (TGA) shall be used herein to downselect polymer molecular weight and ceramic consituent for optimal thermal stability and mechanical durability at temperatures reaching 1000°C. A design of experiments shall be carried out for the down selection process of optimized PDC formulations for ablative and tensile testing of PDC coated reinforcement members. The PDC formulation that exhibits the top overall thermo-oxidative durability and tensile strengths after being exposed to similar heat experienced during AOA maneuvers will be used for prototype fabrication.

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

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