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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. APPLICATION OF G MODEL TECHNOLOGY IN AVIONIC SYSTEMS

    SBC: Bw Technology, Inc.            Topic: N/A

    G MODELS ARE A METHOD FOR REPRESENTING THE ELEVATION OF THE EARTH'S SURFACE THAT PROVIDE SOME SIGNIFICANT ADVANTAGES OVER THE CONVENTIONAL MATRIX FORM USED IN DIGITAL TERRAIN ELEVATION DATA (DTED). AVIONIC SYSTEMS CURRENTLY UNDER R&D IN PROGRAMS SUCH AS ITARS IN THE AVIONICS LABORATORY MAKE EXTENSIVE USE OF DTED. ONE OF THE PRIMARY BENEFITS FROM USING G MODELS IN AVIONIC APPLICATIONS IN PLACE OF D ...

    SBIR Phase I 1990 Department of DefenseAir Force
  2. MACHINE INTELLIGENCE: IMPROVING SPEECH RECOGNITION WITH DYNAMICAL-NEURAL NETWORKS

    SBC: Cognet Systems Inc            Topic: N/A

    OUT OF THE MANY PARAMETERS OF SPEECH RECOGNITION BY MACHINE INTELLIGENCE THERE IS ESPECIALLY ONE KEY ELEMENT THAT MUST HAVE A SOLUTION. THIS INVOLVES THE VARIABILITY OF SPEECH. WE HAVE PROPOSED THAT THE RECENTLY DEVELOPED DYNAMICAL-NEURAL NETWORK IS A CLASS OF MACHINE INTELLIGENCE WHICH HAS PROPERTIES THAT WARRANTS FURTHER RESEARCH AND DEVELOPMENT FOR CONTRIBUTING SOLUTIONS TO THE PROBLEMS OF SPEE ...

    SBIR Phase I 1990 Department of DefenseAir Force
  3. COLD-FLOWED WARHEAD LINERS: CONTROLLED MICROSTRUCTURE FOR ENHANCED PERFORMANCE

    SBC: Cousino Metal Products Inc.            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  4. A PRELIMINARY DESIGN AND ANALYSIS OF AN ADVANCED HEAT REJECTION SYSTEM FOR AN EXTREME ALTITUDE AVCD ENGINE INSTALLED IN A HAARP

    SBC: Dieseldyne Corpon            Topic: N/A

    THE PROPOSED STUDY WILL EVALUATE THE REQUIREMENTS FOR HEAT REJECTION FROM THE VARIOUS SYSTEMS OF AN ULTRA-HIGH ALTITUDEADVANCED VARIABLE CYCLE DIESEL INSTALLED IN A DERIVATIVE AIRFRAME SUITABLE FOR THE AMES ATMOSPHERIC SAMPLING MISSION. A COMBINATION OF CONVECTIVE AND RADIATION HEAT TRANSPORT SYSTEMS WILL BE EVALUATED AND THEN INCORPORATED INTO A DIESEL SIMULATOR CODE FOR PERFORMANCE EVALUATION. C ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  5. INNOVATIVE VULNERABILITY ASSESSMENT TECHNIQUES FOR CONCEPTUAL AIRCRAFT

    SBC: Frontier Technology Inc.            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  6. A SIMPLE AND VERSATILE METHOD FOR THE MEASUREMENT OF SURFACE TENSION

    SBC: H & N Instruments Inc            Topic: N/A

    SURFACE TENSION IS A FUNDAMENTAL PROPERTY OF ALL LIQUIDS. THE SURFACE TENSION OF LIQUIDS DURING PROCESSING AFFECTS THE PROPERTIES OF A VARIETY OF HIGH PERFORMANCE MATERIALS, I.E.: ALLOYS, CERAMICS, COMPOSITES, AND POLYCRYSTALLINE MATERIALS. SURFACE TENSION IS NOT ROUTINELY MEASURED FOR MOST EXPERIMENTAL NEW MATERIALS. THIS IS BECAUSE NO SIMPLE, ACCURATE, YET VERSATILE COMMERCIAL INSTRUMENT EXISTS. ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  7. INCREASED TURBINE ENGINE PERFORMANCE THROUGH MAGNETIC COMPRESSION

    SBC: IAP RESEARCH, INC.            Topic: N/A

    FOR INCREASED TURBINE ENGINE PERFORMANCE HIGHER ROTOR SPEED AND COMPRESSION RATIOS ARE REQUIRED. THE OBJECTIVE OF THIS PROGRAM IS TO REDUCE THE BLADE STRESSES ASSOCIATED WITH INCREASED ROTOR SPEEDS AND COMPRESSION RATIOS. A MAGNETIC SYSTEM APPROACH WILL BE INVESTIGATED. DETAILED MECHANICAL, MAGNETIC, AND THERMAL ANALYSES WILL BE PERFORMED TO DETERMINE FEASIBILITY.

    SBIR Phase II 1990 Department of DefenseAir Force
  8. HIGH-SPEED SUPERCONDUCTING SWITCH

    SBC: IAP RESEARCH, INC.            Topic: N/A

    WE PROPOSE TO DEVELOP A HIGH-SPEED, COMPACT SUPERCONDUCTING SWITCH THAT EXPLOITS UNIQUE PROPERTIES OF THE NEW HT(C) MATERIALS. IN PHASE I WE WILL BUILD AND TEST A SMALL SWITCH TO DEMONSTRATE THE SWITCH TO CONTROL MECHANISM. IN PHASE II WE WILL DEMONSTRATE THE SWITCH IN A CIRCUIT APPLICATION AND DEVELOP PACKAGING CONCEPTS.

    SBIR Phase II 1990 Department of DefenseAir Force
  9. OVERCOMING THE RAILGUN VELOCITY LIMIT

    SBC: IAP RESEARCH, INC.            Topic: N/A

    ELECTROMAGNETIC RAILGUNS HAVE NOT EXCEEDED A VELOCITY LIMIT OF ABOUT 6 KM/S. NEITHER, INCREASING RAILGUN CURRENT NOR INCREASING BARREL LENGTH FOR A GIVEN PROJECTILE MASS, RESULTS IN VELOCITIES GREATER THAN 6 KM/S. WE PROPOSE TO DETERMINE THE FEASIBILITY OF EXCEEDING 6 KM/S WITH A RAILGUN BY MODIFYING THE BARREL AND ARMATURE TO PREVENT PARSITIC SECONDARY CURRENT PATHS. ALL CURRENT WILL BE FORCED TH ...

    SBIR Phase I 1990 Department of DefenseAir Force
  10. VERTICLE/SHORT TAKEOFF AND LANDING (V/STOL) STABILITY AND CONTROL IN GROUND EFFECTS

    SBC: Ksa Technology            Topic: N/A

    IN HOVER THE JET STEAMS FROM A V/STOL AIRCRAFT IMPINGE ON THE GROUND AND SPREAD OUT FROM THE IMPINGEMENT POINT IN RADICALLY FLOWING WALL JETS WITH FOUNTAIN FLOWS BETWEEN THE JETS WHERE THE WALL JETS MEET. THE FOUNTAIN FLOWS TEND TO PRODUCE A LIFTING FORCE BUT THE WALL JET ENTRAINMENT CAUSES AN OPPOSING LIFT LOSS OF SUCKDOWN. AT FORWARD SPEED, AS IN STOL OPERATION, THE FORWARD FLOWING WALL JET IS O ...

    SBIR Phase II 1990 Department of DefenseAir Force
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