SECA, Inc.

Company Information

Company Name
SECA, Inc.
Address
3313 Bob Wallace Ave., Suite 201
Huntsville, AL, 35805-0406
Phone
1 256-534-2008
URL
n/a
DUNS
n/a
Number of Employees
3

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$822,426.00
14
SBIR Phase II
$3,704,777.00
7
Chart code to be here

Award List

  1. 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, ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  2. 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 ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  3. 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 ...

    SBIR Phase I 1989 NavyDepartment of Defense
  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 ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  5. 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 ...

    SBIR Phase II 1992 National Aeronautics and Space Administration
  6. 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 ForceDepartment of Defense
  7. 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
  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. N/A

    Amount: $70,000.00

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  10. 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

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