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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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Swirl Annular Combustor for Aircraft Gas Turbine Engines
Amount: $70,000.00This 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 -
Oblique Detonation Wave Hy-Scram Engine for Hypersonic Propulsion Applications
Amount: $70,000.00The 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 -
AN ADAPTING FINITE ELEMENT MODEL FOR UNSATURATED POROUS MEDIA
Amount: $149,992.00A 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 -
The Design of Sub-Caliber Aero-Thermal-Chemical (ATC) Gun Projectiles for Aerodynamic Stability
Amount: $59,776.00The 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 -
A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications
Amount: $59,986.00This 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 -
A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3
Amount: $74,370.00An 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 -
Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine
Amount: $59,922.00N/A
SBIRPhase I1993Department of Defense Air Force -
Ground Based Scramaccelerator Launcher
Amount: $61,194.00Phase 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 -
AN ADAPTING FINITE ELEMENT MODEL FOR UNSATURATED POROUS MEDIA
Amount: $49,998.00N/A
SBIRPhase I1992Nuclear Regulatory Commission -
AEROACOUSTIC DIFFRACTION AND DISSIPATION BY A SHORT PROPELLER COWL IN SUBSONIC FLIGHT
Amount: $49,998.00N/A
SBIRPhase I1992National Aeronautics and Space Administration