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Award Data
The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.
Download all SBIR.gov award data either with award abstracts (290MB)
or without award abstracts (65MB).
A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.
The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.
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A PROBABILITY DENSITY FUNCTION (PDF) METHOD FOR TURBULENT REACTING FLOWS
SBC: CFD RESEARCH CORPORATION Topic: N/AMODELING METHODS DEVELOPED FOR NON-REACTING TURBULENT FLOWS ARE NOT ABLE TO CAPTURE IMPORTANT INTERACTIONS OF TURBULENCE AND COMBUSTION. AN ALTERNATIVE APPROACH SOLVES AN EQUATION FOR THE JOINT PROBABILITY DENSITY FUNCTION (PDF)OF THE LOCAL VELOCITY AND COMPOSITION, INSTEAD OF SOLVING A SET OF EQUATIONS FOR THEIR FIRST-AND SECOND-ORDER MOMENTS. WHILE PDF METHODS HAVE BEEN PROPOSED IN THE PAST, THE ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
INTERGRATION OF COMBUSTOR AERODYNAMICS AND FUEL SPRAY TO INCREASE TURNDOWN FUEL-AIR RATIO IN SMALL GAS TURBINE COMBUSTORS
SBC: CFD RESEARCH CORPORATION Topic: N/ATHIS PROJECT WILL INTEGRATE COMBUSTOR AERODYNAMICS AND FUEL SPRAY PATTERNS TO ATTAIN HIGH TURNDOWN RATIOS WITHOUT SIGNIFICANTLY MODIFYING CONVENTIONAL COMBUSTOR GEOMETRY. THIS WILL BE ACCOMPLISHED BY: THE CREATION OF TWO DISTINCT ZONES WITHIN THE COMBUSTOR PRIMARY ZONE THAT ARE INDEPENDENTLY FUELED; THE USE OF A DUAL-LIP AIRBLAST FUEL ATOMIZER THAT FUELS ONLY THE CENTRAL RECIRCULATION ZONE AT LOW ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
A 350 DEGREE C 6H SILICON CARBIDE THYRISTOR
SBC: CREE RESEARCH, INC. Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
CONJUGATE SRM HEAT TRANSFER ANALYSIS
SBC: Huntsville Sciences Corp. Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
NEW WIDE-FIELD, MEDIUM-RESOLUTION TELESCOPE WITH ZOOM CAPABILITY FOR PLANETARY
SBC: Korsch Optics Inc Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
MOVING TEMPERATURE GRADIENT HEAT PIPE FURNACE ELEMENT FOR LOW GRAVITY CRYSTAL GROWTH
SBC: Microgravity Systems Inc. Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
RAREFIED GAS EFFECTS ON AEROBRAKING/REENTRY VEHICLES WITH WAKES
SBC: Remtech Inc. Topic: N/AAEROBRAKING VEHICLES (AOTV, ASTV AND VEHICLES TO MARS) ARE GOING TO MAKE SEVERAL PASSES AND DIP LOW IN THE TRANSITIONAL REGIME IN ORDER TO ACHIEVE THE DESIRED REDUCTION IN VELOCITY. EVEN AT THE LOWEST POINT OF THE TRAJECTORY, SURFACE-SLIP EFFECTS PERSIST AND REAL-GAS EFFECTS DUE TO NONEQUILIBRIUM DISSOCIATION AND IONIZATION SIGNIFICANTLY ALTER THE FLOW STRUCTURE. FURTHER, DUE TO IMPINGEMENT OF THE ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
SEMI-RIGID, TAILORABLE, COST-OPTIMIZED NLS HEAT SHIELD
SBC: Remtech Inc. Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
SURFACE ROUGHNESS FEATURES FORMULATION FOR AIRCRAFT ICING
SBC: Remtech Inc. Topic: N/AN/A
SBIR Phase I 1992 National Aeronautics and Space Administration -
RADIATION FROM ADVANCED SOLID ROCKET MOTOR PLUMES
SBC: SECA, Inc. Topic: N/ATHERMAL 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, SHAPE, AND EMISSIVITY; AND HEATING RATES ARE CALCULATED WITH APPROPRIATE VIEW FACTORS FROM THIS SIMPLISTIC PLUME MODEL. ALTHOUGH OTHER EXTENSIVE RELEVANT TECHNOLOGY HAS BEEN DEVELOPED TO DESCRIBE INFRAR ...
SBIR Phase II 1992 National Aeronautics and Space Administration
