ADVANCED PROJECTS RESEARCH, INC.

Address

1925 McKinley Avenue
Suite B
La Verne, CA, 91750 5800

Information

DUNS: 196694640
# of Employees: 11

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: Y

Award Charts




Award Listing

  1. Sensor Validation for Turboshaft Engine Torque Sensors

    Amount: $69,999.00

    We 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 I2008Army Department of Defense
  2. Development of Flow-Field Seeding for Large Wind Tunnels

    Amount: $658,775.00

    The 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 II2008Air Force Department of Defense
  3. Inter-Turbine Burner Technology Demonstration

    Amount: $100,000.00

    The 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
  4. Develop Flow-Field Seeding for Large Tunnels

    Amount: $100,000.00

    The 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 I2006Air Force Department of Defense
  5. Development of a Rugged, Fuel Tank Compatible, Oxygen Concentration Sensor

    Amount: $599,979.00

    The 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
  6. Multi Point Velocity, Density and Temperature Measurements using LITA

    Amount: $70,000.00

    Laser 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
  7. Inter-Turbine Burners for Improved Part Power Performance of Turboshaft Engines.

    Amount: $70,000.00

    he 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 I2004Army Department of Defense
  8. Development of a rugged, fuel tank compatible, oxygen concentration sensor

    Amount: $70,000.00

    We 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
  9. 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 II2002Defense Advanced Research Projects Agency Department of Defense
  10. A High Turn-Down Ratio, Low Emissions Combustor for Gas Turbine Engines

    Amount: $70,000.00

    This 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

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