SOFTWARE & ENGINEERING ASSOC., INC.

Basic Information

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

Company Profile

n/a

Additional Details

Field Value
DUNS: 83152975
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 8


  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 ...

    SBIR Phase I 2010 NavyDepartment of DefenseDepartment of Defense
  2. Innovative Predictive Model for Determining Bore Erosion

    Amount: $729,952.00

    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 ...

    SBIR Phase II 2008 ArmyDepartment of DefenseDepartment of Defense
  3. Innovative Predictive Model for Determining Bore Erosion

    Amount: $69,997.00

    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 ...

    SBIR Phase I 2006 ArmyDepartment of DefenseDepartment 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 ...

    STTR Phase I 2006 Air ForceDepartment of DefenseDepartment of Defense
  5. 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 ...

    SBIR Phase I 2006 Air ForceDepartment of DefenseDepartment of Defense
  6. 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 ...

    STTR Phase I 2006 National Science Foundation
  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 ...

    SBIR Phase II 2004 Department of DefenseAir ForceDepartment of Defense
  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 ...

    SBIR Phase I 2003 Department of DefenseAir ForceDepartment of Defense
  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 ...

    SBIR Phase I 2002 National 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 ...

    SBIR Phase II 2002 NavyDepartment of DefenseDepartment of Defense

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