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Advanced Projects Research, Incorporated
UEI: ESNMMQC4WHQ9
# of Employees: 11
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: Yes
Award Charts
Award Listing
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Sensor Validation for Turboshaft Engine Torque Sensors
Amount: $69,999.00We propose a method that specifically addresses the requirement for helicopter engine torque sensor validation by integrating the engine component level model, model reduction techniques, and real-tim ...
SBIRPhase I2008Department of Defense Army -
Development of Flow-Field Seeding for Large Wind Tunnels
Amount: $658,775.00The Air Force seeks a large production wind tunnel seeding system with full field steering capability. Additionally, the system must offer control of the particle size and density along with minimal ...
SBIRPhase II2008Department of Defense Air Force -
Inter-Turbine Burner Technology Demonstration
Amount: $100,000.00The development of an Inter-Turbine Burner (ITB) for improving the part power performance of small gas turbine engines is proposed. An Inter-Turbine Burner is a second combustor placed between the gas ...
SBIRPhase I2007Department of Defense Air Force -
Develop Flow-Field Seeding for Large Tunnels
Amount: $100,000.00The Air Force seeks a large production wind tunnel seeding system with full field steering capability. Additionally, the system must offer control of the particle size and density along with minimal ...
SBIRPhase I2006Department of Defense Air Force -
Development of a Rugged, Fuel Tank Compatible, Oxygen Concentration Sensor
Amount: $599,979.00The objective of the proposed Phase II effort is to transfer proven sensor technology from the laboratory breadboard to a functional flight-ready prototype for installation in an aircraft fuel tank. I ...
SBIRPhase II2004National Aeronautics and Space Administration -
Multi Point Velocity, Density and Temperature Measurements using LITA
Amount: $70,000.00Laser induced thermal acoustics (LITA) is a nonintrusive, transient-grating optical technique that provides simultaneous high-accuracy measurements of velocity, sound-speed, and thermal diffusivity am ...
SBIRPhase I2004National Aeronautics and Space Administration -
Inter-Turbine Burners for Improved Part Power Performance of Turboshaft Engines.
Amount: $70,000.00he use of an inter-turbine burner for improving the part power performance of small turboshaft engines in proposed. An inter-turbine burner is a second combustor placed between the gas generator exit ...
SBIRPhase I2004Department of Defense Army -
Development of a rugged, fuel tank compatible, oxygen concentration sensor
Amount: $70,000.00We propose to engineer a compact, robust, optically-based sensor for measuring local oxygen concentration in aircraft fuel tanks. This system will utilize absorption of rapidly scanned Vertical Cavity ...
SBIRPhase I2003National Aeronautics and Space Administration -
Gas Turbine Pre-Compressor Cooling Using Water and Oxidizer Injection for Small Access to Space Vehicles
Amount: $593,991.00"The development of a pre-compressor mass injection system for extending the flight Mach number and altitude of conventional military afterburning turbo jet and turbofan engines is proposed. The inje ...
SBIRPhase II2002Department of Defense Defense Advanced Research Projects Agency -
A High Turn-Down Ratio, Low Emissions Combustor for Gas Turbine Engines
Amount: $70,000.00This proposal describes an innovative, high-efficiency, compactcombustor for lean-premixed, low-emissions gas turbine systems andresponds directly to NASA's request for Innovative technologiesrelating ...
SBIRPhase I2002National Aeronautics and Space Administration