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Semiconductor Nanomembrane Based Flight Sensors and Arrays

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CK13P
Agency Tracking Number: 120241
Amount: $125,000.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: T9.01
Solicitation Number: N/A
Solicitation Year: 2012
Award Year: 2013
Award Start Date (Proposal Award Date): 2013-05-23
Award End Date (Contract End Date): 2014-05-22
Small Business Information
158 Wheatland Drive
Pembroke, VA 24136-3645
United States
DUNS: 008963758
HUBZone Owned: Yes
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Hang Ruan
 Principal Investigator
 (540) 626-6266
Business Contact
 Melissa Campbell
Title: Contracts Administrator
Phone: (540) 626-6266
Research Institution
 Virginia Tech
 Melissa Campbell
122 Randolph Hall
Blacksburg, VA 24060-24060
United States

 () -
 Domestic Nonprofit Research Organization

The NASA Phase I program would develop and demonstrate semiconductor nanomembrane (NM) based flight sensors and arrays on flexible substrates, using SOI (Silicon on Insulator) silicon NM technique in combination with our pioneering HybridsilTM copolymer nanocomposite materials. Specifically, ultrathin nanostructured sensor skins with integrated interconnect elements and electronic devices that can be applied to new or existing wind tunnel models for skin friction analysis would be developed. NanoSonic has demonstrated the feasibility of NM transducer materials in such sensor skins for the measurement of flow-induced skin friction and pressure. Early experimental results have compared very favorably with data from other sensor gages.Major improvements from the previous Metal RubberTM based sensor include faster response time and less temperature dependence due to the high carrier mobility with the inorganic NMs. During this NASA STTR program, a semiconductor NM based distributed sensor array will be developed (Phase I) and deployed to measure in-flight (Phase II) the surface properties on an airplane wing surface. The properties that will be measured will include shear stress and pressure. With the high frequency response of the NM sensors (100 kHz), it is possible that laminar to turbulence transition can be detected. In phase I, an existing Mach 0.7 wind tunnel will be used to check out the performance of the sensors.

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

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