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Advanced Projects Research, Incorporated

Company Information
Address
2141 E ALTADENA DR
ALTADENA, CA 91001-2105
United States



Information

UEI: ESNMMQC4WHQ9

# of Employees: 11


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: Yes



Award Charts




Award Listing

  1. Swirl Annular Combustor for Aircraft Gas Turbine Engines

    Amount: $70,000.00

    This proposal describes an innovative Ultra-Low NOx annular swirl combustor concept for aircraft gas turbine engines. The concept is based on previously demonstrated means for creating high mixing rat ...

    SBIRPhase I1994National Aeronautics and Space Administration
  2. Oblique Detonation Wave Hy-Scram Engine for Hypersonic Propulsion Applications

    Amount: $70,000.00

    The Oblique Detonation Wave Hypervelocity Scramjet (ODW Hy-Scram) Engine is applicable to hypersonic flight vehicles that require high Mach Scramjet operation. This project will implement a unique new ...

    SBIRPhase I1994National Aeronautics and Space Administration
  3. AN ADAPTING FINITE ELEMENT MODEL FOR UNSATURATED POROUS MEDIA

    Amount: $149,992.00

    A TWO-DIMENSIONAL NUMERICAL MODEL BASED ON A HYBRID FINITE ELEMENT METHOD WITH MESH ADAPTATION IS PROPOSED TO CALCULATE GROUNDWATER FLOW AND POLLUTANT TRANSPORT IN UNSATURATED POROUS MEDIA. THE ALGORI ...

    SBIRPhase II1993Nuclear Regulatory Commission
  4. The Design of Sub-Caliber Aero-Thermal-Chemical (ATC) Gun Projectiles for Aerodynamic Stability

    Amount: $59,776.00

    The following proposal details an effort required for understanding the in-bore aerodynamic stability of sub-caliber projectiles in aero-thermal- chemical (ATC) guns in order to design stable projecti ...

    SBIRPhase I1993Department of Defense Air Force
  5. A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications

    Amount: $59,986.00

    This proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration i ...

    SBIRPhase I1993Department of Defense Air Force
  6. A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3

    Amount: $74,370.00

    An innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereb ...

    SBIRPhase I1993Department of Defense Air Force
  7. Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine

    Amount: $59,922.00

    N/A

    SBIRPhase I1993Department of Defense Air Force
  8. Ground Based Scramaccelerator Launcher

    Amount: $61,194.00

    Phase I will analyze use of a hypervelocity launcher to provide ahigh mass (2 to 20 kilograms), hypervelocity (4 km\sec) demonstrator for a Theater Missile Defense (TMD) System. Current ballistic powd ...

    SBIRPhase I1992Department of Defense Missile Defense Agency
  9. AN ADAPTING FINITE ELEMENT MODEL FOR UNSATURATED POROUS MEDIA

    Amount: $49,998.00

    N/A

    SBIRPhase I1992Nuclear Regulatory Commission
  10. AEROACOUSTIC DIFFRACTION AND DISSIPATION BY A SHORT PROPELLER COWL IN SUBSONIC FLIGHT

    Amount: $49,998.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration
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