SECA, Inc.

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


Information

DUNS:

# of Employees: 3


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Heated Cloud Rise Model

    Amount: $53,328.00

    N/A

    SBIRPhase I1993Air Force Department of Defense
  2. RADIATION FROM ADVANCED SOLID ROCKET MOTOR PLUMES

    Amount: $499,955.00

    THERMAL LOADS CREATED BY THE PLUMES OF ADVANCED SOLID ROCKETMOTORS ARE NOT PREDICTABLE; SUCH LOADS ARE CURRENTLY OBTAINED FROM EXPERIMENT. TEST DATA ARE CORRELATED BY POSTULATING PLUME TEMPERATURE, SH ...

    SBIRPhase II1992National Aeronautics and Space Administration
  3. CONJUGATE SRM HEAT TRANSFER ANALYSIS

    Amount: $49,954.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration
  4. HEAT TRANSFER IN ROCKET ENGINE COMBUSTION CHAMBERS AND REGENERATIVELY COOLED NOZZLES

    Amount: $500,000.00

    AN IMPROVED HEAT TRANSFER ANALYSIS FOR LIQUID ROCKET ENGINE DESIGN WILL BE DEVELOPED BY USING STATE-OF-THE-ART COMPUTATIONAL FLUID DYNAMICS (CFD) METHODOLOGY TO ACCURATELY DESCRIBE THE RADIATING, COMB ...

    SBIRPhase II1991National Aeronautics and Space Administration
  5. RADIATION FROM ADVANCED SOLID ROCKET MOTOR PLUMES

    Amount: $49,908.00

    N/A

    SBIRPhase I1991National Aeronautics and Space Administration
  6. MODEL DEVELOPMENT FOR EXHAUST PLUME EFFECTS ON LAUNCH STAND DESIGN

    Amount: $499,860.00

    EXISTING MODELS FOR DETERMINING PLUME INDUCED LAUNCH STAND PRESSURE AND THERMAL EFFECTS ARE TOO LABOR AND COMPUTATIONALLY EXPENSIVE TO ROUTINELY APPLY TO DESIGN LAUNCH STANDS AND MISSILE LAUNCHERS. TH ...

    SBIRPhase II1990National Aeronautics and Space Administration
  7. HEAT TRANSFER IN ROCKET ENGINE COMBUSTION CHAMBERS AND REGENERATIVELY COOLED NOZZLES

    Amount: $49,932.00

    N/A

    SBIRPhase I1990National Aeronautics and Space Administration
  8. MODEL DEVELOPMENT FOR EXHAUST PLUME EFFECTS ON LAUNCH STAND DESIGN

    Amount: $49,923.00

    N/A

    SBIRPhase I1989National Aeronautics and Space Administration
  9. CFD ANALYSIS OF GAS TURBINE AGUMENTER IGNITION/BLOWOUT

    Amount: $49,885.00

    A COMPUTATIONAL FLUID DYNAMICS (CFD) ANALYSIS OF IGNITION AND BLOWOUT IN GAS TURBINE AUGMENERS IS PROPOSED IN ORDER TO IMPROVE OUR UNDERSTANDING OF IGNITION AND OF METHODS OF MAINTAINING STABLE COMBUS ...

    SBIRPhase I1989Navy Department of Defense
  10. THE USE OF VARIATIONAL PRINCIPLES IN IMPROVING CFD METHODOLOGY

    Amount: $493,000.00

    THE DEVELOPMENT OF A COMPUTATIONAL FLUID DYNAMICS (CFD) MODEL BASED ON VARIATIONAL PRINCIPLES AND USED TO SIMULATE AERODYNAMIC FLOWS IS PROPOSED. THE CFD MODEL WILL BE DESIGNED TO DESCRIBE TURBULENT, ...

    SBIRPhase II1988National Aeronautics and Space Administration

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