Company Information
Address 8940 STATE ROUTE 108 STE L
COLUMBIA, MD, 21045-2129


DUNS: 018413208

# of Employees: 30

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. High-Fidelity Design Tools and Technologies for High-Pressure Heavy Fuel Injectors

    Amount: $100,000.00

    In propulsion systems, liquid fuel is atomized and burned in a way that maximizes engine efficiency and minimizes emissions. To accomplish this task, it is necessary to design injectors and nozzles th ...

    SBIRPhase I2017Department of Defense Army
  2. Ignition Modeling for Present and Future Combustors and Augmentors

    Amount: $125,000.00

    The ability to predict the ignitibility potential of a combustor at various operating conditions is not practical at this time due to the complexity of this process. Ignition within a gas turbine comb ...

    STTRPhase I2017Department of Defense Navy
  3. Physics-Based and Computationally Efficient Combustion Chemistry Modules with Acceptable Uncertainty for Air Force Relevant Hydrocarbon Fuels

    Amount: $149,998.00

    The overall goal of this project is to validate and enhance the latest available combustion kinetics models for fuels that are of relevance to the Air Force propulsion systems. To achieve this goal, ...

    STTRPhase I2017Department of Defense Air Force
  4. Improved Reaction Models for Petroleum and Alternative JP-5/8 Fuels

    Amount: $749,972.00

    ABSTRACT: In recent years, diversification of energy dependence on foreign oil has attracted the use of alternative fuels such as the Fischer-Tropsch jet fuels and hydro-treated renewable jet fuels. ...

    SBIRPhase II2015Department of Defense Air Force
  5. Active Control of a Scramjet Engine

    Amount: $150,000.00

    ABSTRACT: The hydrocarbon-fueled scramjet is capable of providing hypersonic air-breathing propulsion for high-speed applications. The effective operation of high-speed air-breathing engines (ram- and ...

    STTRPhase I2015Department of Defense Air Force
  6. Prediction and Measurement of the Soot Build-Up in Film-Cooled Rocket Engines

    Amount: $150,000.00

    ABSTRACT: The need for improved performance of liquid rocket engines requires efficient wall cooling technologies to mitigate high heat fluxes from hot combustion gases to the engine wall in the thrus ...

    STTRPhase I2015Department of Defense Air Force
  7. Low-Weight, High-Temperature Passive Damping System for Afterburners

    Amount: $149,999.00

    ABSTRACT: Afterburners operate under a wide range of operating conditions and hence they are likely to encounter conditions at which combustion (thermoacoustic) instabilities occur. Therefore, metho ...

    SBIRPhase I2015Department of Defense Air Force
  8. Physical Sub-Model Development for Turbulence Combustion Closure

    Amount: $749,998.00

    ABSTRACT: The U. S. Air Force needs turbulent combustion models that can be used to simulate combustion in actual propulsion systems at both design and off-design conditions, not models that are only ...

    STTRPhase II2015Department of Defense Air Force
  9. Computational Modeling of Coupled Acoustic and Combustion Phenomena Inherent to Gas Turbine Engines

    Amount: $748,211.00

    ABSTRACT:The pressure oscillations associated with thermoacoustic combustion instabilities are a serious hazard to combustion systems such as gas-turbine-engine combustors, augmentors / afterburners, ...

    SBIRPhase II2015Department of Defense Air Force
  10. Nonequilibrium Plasma-Assisted Combustion-Efficiency Control in Vitiated Air

    Amount: $150,000.00

    ABSTRACT: The ability of plasmas to modify combustion has been known for more than 50 years. Recent advances in plasma generation technology and measurement diagnostics have led to extensive efforts ...

    STTRPhase I2014Air Force Department of Defense

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