SECA, Inc.

Company Information
Address 3313 Bob Wallace Ave., Suite 201
Huntsville, AL, 35805-0406



# of Employees: 3

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. Integration of High-Pressure Combustion Experiments and Simulations

    Amount: $69,996.00

    An innovative method for integrating experimental design with computational flowfield methodology for developing advanced liquid rocket combustors is proposed. Despite dramatic advancements in computa ...

    SBIRPhase I2002National Aeronautics and Space Administration
  2. N/A

    Amount: $70,000.00


    SBIRPhase I2000National Aeronautics and Space Administration
  3. Three-Dimensional, Three Phase Combustion

    Amount: $619,956.00


    SBIRPhase II1998National Aeronautics and Space Administration
  4. Three-Dimensional, Three Phase Combustion

    Amount: $69,985.00


    SBIRPhase I1997National Aeronautics and Space Administration
  5. Propulsion Chemistry for CFD Applications

    Amount: $599,878.00

    SECA, Inc. proposes to develop a series of computational modules which describe real fluid thermodynamics and physical properties that are designed to be easily incorporated in computational fluid dyn ...

    SBIRPhase II1995National Aeronautics and Space Administration
  6. Soot Formation In Rocket Propulsion Systems

    Amount: $69,984.00


    SBIRPhase I1995National Aeronautics and Space Administration
  7. Prediction of Combustion Efficiency in a Hybrid Motor

    Amount: $69,708.00

    SECA, Inc. with the assistance of AMROC, Inc. proposes to develop the methodology required to analytically predict the combustion efficiency of operational hybrid rocket motors from basic test data ch ...

    SBIRPhase I1994National Aeronautics and Space Administration
  8. Propulsion Chemistry for CFD Applications

    Amount: $69,958.00


    SBIRPhase I1994National Aeronautics and Space Administration
  9. Heated Cloud Rise Model

    Amount: $492,128.00

    The rise of launch clouds to stabilization is forced by an altitude varying distribution of momention and buoyancy (temperature). In most of the plume, the temperature excess over that of the atmosphe ...

    SBIRPhase II1994Air Force Department of Defense
  10. Radiation-Convection Coupling in Rocket Motor and Plume Analysis

    Amount: $49,990.00


    SBIRPhase I1993National Aeronautics and Space Administration

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