SBIR/STTR Research Award

Oxygen-Independent Pressure Sensitive Paint

Award identifier f300af290bd653c1b24ca3e1a138dcafbd03d98436dca7b327059f0b0afe114eAwarding agency National Aeronautics and Space Administration

Award amount

$749,955

Program and phase

SBIR · Phase II

Award year

2015

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
INTELLIGENT OPTICAL SYSTEMS, INC.
Proposal award date
2015-05-01
Contract end date
2017-04-30
UEI
NLDHG92SMX37
Solicitation number
Not reported
Topic code
A4.01

Research abstract

Pressure sensitive paint (PSP) systems are excellent tools for performing global pressure measurements in aerodynamic testing, especially in wind tunnel studies. The major limitation of PSP for pressure mapping is its dependence on an oxygen-containing flow, since those paints are actually oxygen sensors. Intelligent Optical Systems (IOS) is developing a unique coating in which fluorescence quenching can form high resolution images of the true pressure distribution on surfaces in transonic flow in oxygen-free atmospheres. The fluorescence in these unique coatings depends directly on absolute pressure, and oxygen permeation into the coatings is not required. The new coating, however, is completely compatible with the "legacy" (oxygen sensing) visualization equipment used in current transonic test facilities. With this novel pressure sensing technology, coating materials can be used that are not useful for oxygen-based PSPs, and coatings that can meet requirements not achievable with classical paints, like operation at extremely low temperature or in highly contaminated environments. In Phase I, IOS has created the oxygen-insensitive pressure-sensitive coating materials, and applied them to glass and stainless steel test coupons. The fluorescence emission lifetime and intensity of these test samples were measured at varying static pressures under pure nitrogen, showing significant correlation with pressure in the range studied (from 0.05 to 14.7 psi), and excellent repeatability. This sets the stage for Phase II development and delivery of a complete temperature-compensated true ambient pressure sensitive paint system that can be used to characterize flow around structures in hypersonic wind tunnels. At the end of Phase II, the coatings will have been tested at relevant environments (TRL5), and will be available for NASA to begin testing in a high-fidelity laboratory environment (TRL6).

Technology keywords

Not reported

Other awards by this recipient

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Awards with the same topic code

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Research funding history

264 SBIR/STTR records share this UEI (1998–2025). Reported award amounts total $77,140,779. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Health and Human Services, National Aeronautics and Space Administration, Department of Energy, Environmental Protection Agency, Department of Agriculture

Agency intelligence

National Aeronautics and Space Administration

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