SECA, Inc.

Basic Information

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

Company Profile

n/a

Additional Details

Field Value
DUNS: n/a
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 3


  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 ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  2. N/A

    Amount: $70,000.00

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  3. Three-Dimensional, Three Phase Combustion

    Amount: $619,956.00

    N/A

    SBIR Phase II 1998 National Aeronautics and Space Administration
  4. Three-Dimensional, Three Phase Combustion

    Amount: $69,985.00

    N/A

    SBIR Phase I 1997 National 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 ...

    SBIR Phase II 1995 National Aeronautics and Space Administration
  6. Soot Formation In Rocket Propulsion Systems

    Amount: $69,984.00

    N/A

    SBIR Phase I 1995 National Aeronautics and Space Administration
  7. 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 ...

    SBIR Phase II 1994 Air Force Department of Defense
  8. 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 ...

    SBIR Phase I 1994 National Aeronautics and Space Administration
  9. Propulsion Chemistry for CFD Applications

    Amount: $69,958.00

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
  10. Radiation-Convection Coupling in Rocket Motor and Plume Analysis

    Amount: $49,990.00

    N/A

    SBIR Phase I 1993 National Aeronautics and Space Administration

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