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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. EMERGING TECHNOLOGIES RESULTING IN LIGHTER AIRCRAFT WEIGHT INCREASED ENGINE PERFORMANCE (ISP) AND IMPROVED DESIGN TOOLS

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  2. DETERMINATION OF EFFECTS OF INTEROPERABILITY ISSUES ON INTRATHEATER AIRLIFT

    SBC: AMERICAN METAL PROCESSING, INC.            Topic: N/A

    BETTER METHODS TO DELIVER AND DISSEMINATE CARGO ARE NECESSARY TO FULLY EXPLOIT THE CAPABILITIES OF FUTURE INTRATHEATER AIRLIFTERS. THE ARMY'S AND AIR FORCE RENEWED EMPHASIS ON MOBILITY WILL REQUIRE GREATER PRODUCTIVITY BY TRANSPORTATION RESOURCES TO ACHIEVE NATIONAL OBJECTIVES. THE NECESSITATES A MORE THOROUGHLY-INTEGRATED TRANSPORTATION NETWORK. ADVANCED TECHNOLGIES, MATERIALS, AND INNOVATIVE ENG ...

    SBIR Phase I 1990 Department of DefenseAir Force
  3. STRESS ANALYSIS OF HYPERVELOCITY MODELS UNDER HIGH G-LOADS

    SBC: APTEK, Inc.            Topic: N/A

    THE OBJECTIVE OF THE PROPOSED WORK IS TO ANALYZE THE HYPERVELOCITY MODELS TESTED AT ARNOLD ENGINEERING DEVELOPMENT CENTER TO DETERMINE THE CAUSE OF NOSETIP FRACTURES. WE WILL ACCOMPLISH THIS GOAL BY PERFORMING TWOAND THREE-DIMENSIONAL FINITE ELEMENT ANALYSES OF THE HYPERVELOCITY MODEL USING DYNA2D AND DYNA3D. IF NECESSARY, WE WILL ALSO DO HYDRODYNAMIC ANALYSES OF THE GAS EXPANSION WHICH DRIVES THE ...

    SBIR Phase II 1990 Department of DefenseAir Force
  4. NONDESTRUCTIVE TESTS AND EVALUATION TECHNIQUES FOR SOLID ROCKET MOTORS

    SBC: APTEK, Inc.            Topic: N/A

    THE PROPOSED RESEARCH PROGRAM WILL PROVIDE AN EVALUATION TOOL FOR ASSESSING THE EFFECTS OF MANUFACTURING AND IN-SERVICE MATERIAL ANOMALIES ON SUBSEQUENT SOLID ROCKET MOTOR PERFORMANCE. THE EVALUATION TOOL CONSISTS OF A NONLINEAR FINITE ELEMENT PROGRAM WITH A COMPOSITE DAMAGE AND FAILURE CONSTITUTIVE MODEL. THE EVALUATION TOOL WILL BE VERIFIED BY CORRELATION WITH LABORATORY TESTS OF DESIGNATED COMP ...

    SBIR Phase I 1990 Department of DefenseAir Force
  5. TELEPRESENT MASTER/SLAVE TOOLS WITH FORCE AND TACTILE FEEDBACK

    SBC: Begej Corp.            Topic: N/A

    THE OVERALL OBJECTIVE OF THE PHASE I WORK SHALL BE TO DESIGN AND FABRICATE TELEPRESENT MASTER/SLAVE (M/S) TOOLS CAPABLE OF PROVIDING FORCE AND TACTILE FEEDBACK TO THE HAND OF A HUMAN OPERATOR. THIS WORK SHALL INCORPORATE THE EXTENSIVE PREVIOUS DEVELOPMENT ACTIVITIES AT BEGEJ CORPORATION IN THE AREAS OF TACTILE SENSORS AND TACTILE DISPLAYS. THE SCOPE OF THE PHASE I WORK INCLUDES: (1) DESIGN AND FAB ...

    SBIR Phase I 1990 Department of DefenseAir Force
  6. RETRODIRECTIVE FLIGHT TEST ARTICLE INSTRUMENTATION ANTENNA

    SBC: Brehn Corp            Topic: N/A

    A FAMILY OF ELECTRONICALLY STEERED CIRCULAR PHASED ARRAY ANTENNAS ARE CONFIGURED FOR USE ON SPINNING RE-ENTRY VEHICLES (RV). THIS TECHNIQUE ALLOWS RVS FROM SIX INCHES TO TEN FEET DIAMETER TO ACHIEVE GREATLY INCREASED PERFORMANCE COMPARED TO PRESENT SYSTEMS: CONTINUOUS RANGE SAFETY ACHIEVED THROUGHOUT RV FLIGHT; SIGNIFICANTLY HIGHER DATA RATES FROM IMPROVED DATA MONITORING; REQUIRED SPATIAL COVERAG ...

    SBIR Phase I 1990 Department of DefenseAir Force
  7. NUMERICAL MODELLING OF KINETICS-TURBULENCE INTERACTION IN HIGH MACH NUMBER FLOWS

    SBC: Cambridge Hydrodyn Inc            Topic: N/A

    WE PROPOSE TO DEVELOP METHODS TO SOLVE ONE OF THE CRITICAL PROBLEMS OF TURBULENCE MODELLING INVOLVED IN HYPERSONIC FLOW IN WHICH ALL TRADITIONALLY USED TURBULENCE MODELS FAIL, NAMELY MODELLING OF KINETIC MIXING AND CHEMICAL REACTION PROCESSES IN HIGH MACH NUMBER (MA-25) TURBULENT FLOWS. WE PROPOSE TO DEVELOP DIFFERENTIAL TRANSPORT MODELS BASED ON OUR NEW RENORMALIZATION-GROUP (RNG) THEORY FOR TURB ...

    SBIR Phase II 1990 Department of DefenseAir Force
  8. DEVELOPMENT OF HYBRID MODEL FOR ASSESSING CONCENTRATIONS OF TOXIC EFFLUENT AT AIR FORCE INSTALLATIONS

    SBC: Cermak Peterka Petersen Inc            Topic: N/A

    PRESENT COMPUTER MODELS USED TO PREDICT VAPOR CLOUD LENGTH, CONCENTRATION AND DURATION AT AIR FORCE INSTALLATIONS DO NOT PROPERLY ACCOUNT FOR THE EFFECTS OF STRUCTURES. STRUCTURES CAN ACT TO TRAP THE CLOUD AND INCREASE THE CLOUD DIMENSIONS, THEREBY POSSIBLY REDUCING DOWNWIND CONCENTRATIONS AND INCREASING THE CLOUD'S LATERAL EXTENT. RECENT RESEARCH CONDUCTED BY CPP HAS SHOWN THAT THE TRAPPING AND I ...

    SBIR Phase I 1990 Department of DefenseAir Force
  9. MULTILEVEL ADAPTIVE METHODS FOR THE EAGLE CODE

    SBC: Colorado Research Development            Topic: N/A

    THE EAGLE GRID GENERATION CODE IS A WIDELY USED SOFTWARE TOOL FOR GENERATING COMPUTATIONALLY UNIFORM GRIDS THAT FIT IRREGULAR PHYSICAL DOMAINS. BASED ON ELLIPTIC GRID GENERATION, IT USES A BLOCKSTRUCTURED APPROACH TO ACCOMMODATE VERY IRREGULAR REGIONS AND POINT DISTRIBUTION FUNCTIONS TO REDUCE FLOW-SOLVER TRUNCATION ERROR. IT ALSO INCORPORATES AS EULER SOLVER FOR INVISCID FLOW CALCULATIONS. WHILE ...

    SBIR Phase I 1990 Department of DefenseAir Force
  10. AERODYNAMIC ANALYSIS OF SUBSONIC VERTICAL TAKE-OFF AND LANDING AIR VEHICLE

    SBC: Corpdray Research Inc.            Topic: N/A

    THE ADVENT OF THE CORDRAY ROTARY ENGINE HAS MADE POSSIBLE SUBSTANTIAL INCREASES IN THE POWER TO WEIGHT RATIO AVAILABLE TO THE AIRCRAFT DESIGNER. ENGINE SELECTION IS HISTORICALLY THE PRIMARY DETERMINATIVE OFVEHICLE DESIGN AND PERFORMANCE. THE AVAILABILITY OF THIS ENGINE ALONGWITH ADVANCES IN COMMAND AND CONTROL ELECTRONICS MAKES POSSIBLE A NEW CLASS OF VEHICLE CAPABLE OF VERTICAL TAKE OFF AND THEN ...

    SBIR Phase II 1990 Department of DefenseAir Force
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