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Friction-Sensing Retroreflector Array Patches (FRAP)

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CB37P
Agency Tracking Number: 075176
Amount: $99,981.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A4.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-02-06
Award End Date (Contract End Date): 2008-08-05
Small Business Information
4325-B Forbes Blvd.
Lanham, MD 20706-4854
United States
DUNS: 076337877
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 John Kline
 Principal Investigator
 (732) 329-3700
 kline@researchsupport.com
Business Contact
 Christopher Rollins
Title: Vice President
Phone: (301) 306-0010
Email: rollins@researchsupport.com
Research Institution
N/A
Abstract

Research Support Instruments, Inc. (RSI) proposes to develop the Friction-Sensing Retroreflector Array Patches (FRAP), a technology that will measure the shear stress distribution on aerodynamic surfaces in ground test facilities with high resolution, sensitivity, and bandwidth. Unlike the oil-film interference method, FRAP patches will not be thinned as a function of time during a test. No knowledge of the streamlines of the flow will be needed in order to calculate the local stress distribution; this will avoid the tracers needed with the oil-film interference approach. Flexible patches of FRAP arrays, inexpensive due to simple, mass-production-compatible microfabrication techniques, will be interrogated using a light source and camera. FRAP will be independent of the flow species and applied as a very thin, flexible, adhesive material. The Phase I goals will be to design sensors, develop a microfabrication technique and use it to fabricate prototype units, demonstrate feasibility, and select the most promising design for Phase II development. In Phase II, the prototype units will be field-demonstrated at NASA facilities, with manufacturing issues and realistic operating conditions addressed. The result will be a product that will address a critical NASA instrumentation need.

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

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