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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.

Displaying 1 - 10 of 288 results
 
  • Record 1 TO 288

  1. THE DEVELOPMENT OF EXTREMELY FAST RISC-BASED ALUS FOR CHARACTER STRING PROCESSING

    SBC: Accelerated Processors Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration

  2. A DISPLAY TECHNIQUE IS DESCRIBED WHICH HAS DESIRABLE PROPERTIES FOR PRESENTATION OF THREE-DIMENSIONAL INFORMATION.

    SBC: Advanced Dimensional Displays            Topic: N/A

    A DISPLAY TECHNIQUE IS DESCRIBED WHICH HAS DESIRABLE PROPERTIES FOR PRESENTATION OF THREE-DIMENSIONAL INFORMATION. THE DISPLAY CAN BE UNDATED IN REAL-TIME THROUGH THE USE OF ELECTRICALLY-ADDRESSED SPATIAL LIGHT MODULATORS. IT IS AUTOSTEREOSCOPIC IN THAT A VIEWER CAN OBTAIN HORIZONTAL PARALLAX AND BY MOVING TO DIFFERENT PARTS OF THE VIEWING AREA CAN SEE DIFFERENT VIEWS OF THE DISPLAYEDOBJECT. IN TH ...

    SBIR Phase I 1985 National Aeronautics and Space Administration

  3. FUEL ATOMIZATION AND AIR-FUEL INTERACTINS IN A TURBULENT ENVIRONMENT

    SBC: Aerometrics Inc.            Topic: N/A

    EXPERIMENTAL INVESTIGATTIONS ARE PROPOSED ON FUEL ATOMIZATION AND AIR-FUEL INTERACTIONS IN A TURBULENT ENVIRONMENT. UNDER THE PROPOSED PROGRAM THE TWO BASIC AREAS OF RESEARCH WILL BE ADDRESSED; COLD FLOW SPRAY CHARACTERIZATIONS IN A TURBULENT FLOW FIELD WITH AND WITHOUTEVAPORATION AND DROP DRAG DETERMINATIONS WITHIN A POLYDISPERSION. DETAILED SPRAY DROP SIZE AND VELOCITY AND GASEOUS FLOW TURBULENC ...

    SBIR Phase II 1987 National Aeronautics and Space Administration

  4. DIAGNOSTICS DEVELOPMENT FOR THE CHARACTERIZATION OF LIQUID FUEL ROCKET ENGINE INJECTOR ATOMIZATION

    SBC: Aerometrics Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration

  5. FUEL ATOMIZATION AND AIR-FUEL INTERACTINS IN A TURBULENT ENVIRONMENT

    SBC: Aerometrics Inc.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration

  6. A RELIABLE, MECHANICAL CRYOCOOLER FOR 80 K COOLING IN SPACE

    SBC: Alabama Cryogenic Engineering, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration

  7. TETHER DEPLOYMENT MONITORING SYSTEM

    SBC: ANCO ENGINEERS, INC.            Topic: N/A

    THE FEASIBILITY AND ECONOMICS OF USING TETHERS FOR STATION-KEEPING OR SLING LAUNCH OF PAYLOADS IS HIGHLY DEPENDENT ON THE RELIABLE CONTROL OF THE TETHER ITSELF IN ANENVIRONMENT. THE PROPOSED TETHER DEPLOYMENT MONITORING SYSTEM (TDMS) WOULD PROVIDE DATA ON THE TETHER'S CONDITION, GUIDANCE IMFORMATION, AND EARLY WARNING ON POSSIBLE FAILURE CONDITIONS. INSTRUMENT PACKAGE WOULD BE DEPLOYED ALONG THE T ...

    SBIR Phase II 1987 National Aeronautics and Space Administration

  8. TETHER DEPLOYMENT MONITORING SYSTEM

    SBC: ANCO ENGINEERS, INC.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration

  9. INSTRUMENTED TORQUE WRENCH

    SBC: ANCO ENGINEERS, INC.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration

  10. DIAGNOSTIC TECHNIQUE TO IDENTIFY AIRBORNE AND STRUCTUREBORNENOISE COMPONENTS

    SBC: Astron Research & Engineering            Topic: N/A

    THERE IS A CRITICAL NEED TO MEASURE STRUCTUREBORNE NOISE TRANSMISSION IN AIRCRAFT, PARTICULARLY THOSE POWERED BY THE ADVANCED TURBOPROP. IT IS PROPOSED THAT A STRUCTUREBORNE INTENSITY MEASUREMENT PROCEDURE BE FORMULATED AND DEVELOPED FOR IN-FLIGHT APPLICATION. THE PROCEDURE WOULD INCLUDE CONSIDERATION OF FLEXURAL, LONGITUDINAL AND ROTATIONAL WAVE COMPONENTS, SINCE THEY ALL CONTRILUTE TO THE TRANSM ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
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