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Award Data

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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.

  1. JOINED WING AIRCRAFT

    SBC: Aca Industries, Inc.            Topic: N/A

    THE JOINED WING IS A NEW TYPE OF AIRCRAFT CONFIGURATION WHICH EMPLOYS TANDEM WINGS ARRANGED TO FORM DIAMOND SHAPES IN BOTH PLAN AND FRONT VIEWS. WIND TUNNEL TESTS AND FINITE- ELEMENT STRUCTURAL ANALYSES SHOW THAT THE JOINED WING PROVIDES THE FOLLOWING ADVANTAGES OVER A COMPARABLE CONVENTIONAL WING: LIGHTER WEIGHT AND HIGHER STIFFNESS, LESSINDUCED DRAG, LOWER WAVE DRAG, HIGHER TRIMMED MAXIMUM LIFT ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  2. AUTOMATIC CONTAMINATION EVALUATOR FOR OPTICAL SURFACES

    SBC: Acton Research Corp.            Topic: N/A

    RECENT SHUTTLE FLIGHTS HAVE SHOWN THAT SIGNIFICANT TEMPORARYOR PERMANENT DEGRADATION OF OPTICAL SURFACES CAN OCCUR IN FLIGHT. SEVERAL OSMIUM-COATED SAMPLES, FLOWN ON SHUTTLE FLIGHT STS 5, EXPERIENCED A PERMANENT LOSS OF REFLECTIVITY BY FACTORS OF 2-3 IN THE VACUUM ULTRAVIOLET PORTION OF THE SPECTRUM. OTHER COATING MATERIALS AND WINDOWS CARRIED ABOARD EARLIER SHUTTLE FLIGHTS SUFFERED LESS OR EVEN N ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  3. ADIABATIC WANKEL TYPE ROTARY ENGINES

    SBC: ADIABATICS INC            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration
  4. SPECTROMETERS

    SBC: Aracor            Topic: N/A

    FOR THE CLASS OF DNA NUCLEAR WEAPONS EFFECTS SIMULATOR KNOWN AS THE PLASMA RADIATING SOURCE (PRS), HIGH RESOLUTION X-RAY SPECTROSCOPY DIAGNOSTIC MEASUREMENTS PROVIDE CRITICAL INFORMATION BOTH FOR CHARACTERIZATION OF THE TEST-OBJECT RADIATION ENVIRONMENT AND FOR OPTIMIZATION OF THE SOURCE. PRESENT PRS HIGH RESOLUTION X-RAY SPECTROMETERS RECORD DATA ON PHOTOGRAPHIC FILM, THE PROCESSING AND ANALYSIS ...

    SBIR Phase I 1984 Department of DefenseDefense Threat Reduction Agency
  5. COMMERCIAL SAPPHIRE SURFACES CONTAIN BURIED DAMAGE WHICH HAS A DELETERIOUS INFLUENCE ON SOS LAYERS GROWN THEREON.

    SBC: Aracor            Topic: N/A

    COMMERCIAL SAPPHIRE SURFACES CONTAIN BURIED DAMAGE WHICH HAS A DELETERIOUS INFLUENCE ON SOS LAYERS GROWN THEREON. THE DEFECTS IN THE SILICON LAYERS RESULT IN A REDUCED YIELD OF DEVICES AND PERFORMANCE LIMITATIONS. MUCH OF THE DAMAGE IN THE SAPPHIRE SURFACE IS PRODUCED BY THE POLISHING STEP, WHICH EMPLOYS AN ABRASIVE PAD IN CONTACT WITH THE SAPPHIRE SURFACE. AN IMPROVED POLISHING PROCESS HAS BEEN E ...

    SBIR Phase I 1984 Department of DefenseDefense Threat Reduction Agency
  6. THIS STUDY WILL DETERMINE CLOUD PROPERTIES FROM LANDSAT 4 THEMATIC MAPPER (TM) DATA BY COMBINING A SPATIAL COHERENCE APPROACH WITH A VARIETY OF CLOUD PARAMETER RETRIEVAL METHODS.

    SBC: ATMOSPHERIC & ENVIRONMENTAL RESEARCH, INC.            Topic: N/A

    THIS STUDY WILL DETERMINE CLOUD PROPERTIES FROM LANDSAT 4 THEMATIC MAPPER (TM) DATA BY COMBINING A SPATIAL COHERENCE APPROACH WITH A VARIETY OF CLOUD PARAMETER RETRIEVAL METHODS. THE TM HAS SEVEN SPECTRAL BANDS WHICH, IN PRINCIPLE, ALLOW CLOUD AMOUNT, HEIGHT, PHASE, AND THICKNESS TO BE RETRIEVED. CLOUD PARTICLE SIZE MAY ALSO BE RETRIEVABLE. THE SPATIAL COHERENCE APPROACH WILL ACCOUNT FOR PARTIAL B ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  7. RAYLEIGH SCATTERING AS A HIGH TEMPERATURE COMBUSTION DIAGNOSTIC METHOD

    SBC: AERODYNE RESEARCH INC            Topic: N/A

    THIS PROJECT EVALUATES THE USE OF RAYLEIGH SCATTERING TECHNIQUES FOR USE AS A TEMPERATURE MONITOR IN THE SEVERE ENVIRONMENT OF GAS TURBINES. POTENTIAL ADVANTAGES OF THIS TECHNIQUE OVER ALL OTHER PRESENTLY USED METHODS ARE HIGH ACCURACY (+/-10K), EASE OF INSTALLATION, HIGH SPATIAL AND TEMPORAL RESOLUTION, AND NONINTRUSIVE OPERATION. THIS PHASEOF THE PROGRAM CONSISTS OF DETAILED FEASIBILITY CALCULAT ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  8. THIS IS A PROJECT TO ESTABLISH THE FEASIBILITY OF A TECHNIQUE FOR FORMING HOLOGRAMS FOR THREE DIMENSIONAL IMAGES OF COMPUTER-GENERATED OBJECTS IN REAL-TIME POINT BY POINT.

    SBC: AERODYNE RESEARCH INC            Topic: N/A

    THIS IS A PROJECT TO ESTABLISH THE FEASIBILITY OF A TECHNIQUE FOR FORMING HOLOGRAMS FOR THREE DIMENSIONAL IMAGES OF COMPUTER-GENERATED OBJECTS IN REAL-TIME POINT BY POINT. THIS PROPRIETARY TECHNIQUE IS A METHOD FOR QUICKLY MOVING POINTS OF LIGHT THROUGH A THREE-DIMENSIONAL OBJECT VOLUME. THIS NEW METHOD, ALONG WITH THE YOUNG TECHNOLOGY OF REAL-TIME THERMO-PLASTIC RECORDING MATERIALS, WILL OVERCOME ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  9. AN OPEN PATH DIODE LASER FLUX METER FOR TRACE GASES OF BIOGENIC ORIGIN

    SBC: AERODYNE RESEARCH INC            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration
  10. OPTIMAL SILICON CARBIDE PRODUCTION

    SBC: AERODYNE RESEARCH INC            Topic: N/A

    N/A

    SBIR Phase I 1984 National Aeronautics and Space Administration
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