SOFTWARE & ENGINEERING ASSOC., INC.

Company Information
Address 1802 N. Carson Street
Suite 200
Carson City, NV, 89701-1238


Information

DUNS: 83152975

# of Employees: 8


Ownership Information

Hubzone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Acoustic Stability Prediction In Solid Rocket Motors

    Amount: $79,970.00

    The ability for engineers to assess the impact of their preliminary design of solid rocket motor (SRM) performance and combustion stability is the focus of this proposal. The SRMs of the future will b ...

    SBIRPhase I2010Navy Department of Defense
  2. Innovative Predictive Model for Determining Bore Erosion

    Amount: $729,953.00

    New requirements for modern gun systems have greatly increased the propellant flame temperature and reactivity of the combustion products. As a result, thermochemical erosion can greatly reduced the ...

    SBIRPhase II2008Army Department of Defense
  3. Innovative Predictive Model for Determining Bore Erosion

    Amount: $119,975.00

    New requirements for modern gun systems have greatly increased the propellant flame temperature and reactivity of the combustion products. As a result, thermochemical erosion can greatly reduced the ...

    SBIRPhase I2006Army Department of Defense
  4. Aluminum Agglomeration and Trajectory in Solid Rocket Motors

    Amount: $99,819.00

    The demand for higher performance rocket motors at a reduced cost requires continuous improvements in understanding and controlling propellant combustion. Numerous examples are available where seemin ...

    STTRPhase I2006Air Force Department of Defense
  5. STTR Phase I: Multi-Dimensional Hydrodynamic Stability Analysis Tool for Solid Rocket Motors

    Amount: $99,973.00

    This Small Business Technology Transfer (STTR) Phase I project is to determine the feasibility of developing a hydrodynamic combustion stability analysis design tool for rockets, gas turbines, and lar ...

    STTRPhase I2006National Science Foundation
  6. Advanced Rocket Propulsion Technologies

    Amount: $99,909.00

    A modeling and experimental program is proposed with the goal of reducing the mean size of metal oxide droplets in the exhaust of solid propellant rocket motors (SRMs). The proposed effort looks at a ...

    SBIRPhase I2006Air Force Department of Defense
  7. Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

    Amount: $749,973.00

    Liquid rocket engines may be run for repeatedly over extended periods of time, requiring active cooling. An efficient means of cooling LRE nozzles involves using the liquid fuel or oxidizer itself to ...

    SBIRPhase II2004Department of Defense Air Force
  8. Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

    Amount: $99,947.00

    Design of a high performance hydrocarbon liquid rocket engine (LRE) requires a thorough understanding of the heat transfer and cooling requirements of LRE's. An efficient cooling system is crucial in ...

    SBIRPhase I2003Department of Defense Air Force
  9. An Innovative Method of NOX Reduction Through Fuel Additives for the UEET Program

    Amount: $99,252.00

    The opportunity addressed in this proposal is to transfer a fuel-additive technology developed for NOx and particulate matter reduction in diesel fuels, to applications in ultra-efficient jet engine f ...

    SBIRPhase I2002National Aeronautics and Space Administration
  10. Modeling of Composite Solid Propellant Combustion

    Amount: $450,000.00

    Chemical kinetics based solid propellant combustion predictive capabilities have developed to the point where it is possible to compute combustion properties of solid propellants. Specifically, burni ...

    SBIRPhase II2002Navy Department of Defense

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