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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. A CATALYTIC THERMAL MANAGEMENT SYSTEM FOR HYDROGEN-FUELED INJECTION VEHICLES

    SBC: Accel Catalysis Inc.            Topic: N/A

    A COOLING STRATEGY UTILIZING THE ENDOTHERMICITY OF THE PARA- TO ORTHO-HYDROGEN CONVERSION HAS POTENTIAL FOR MEETINGTHE REQUIREMENTS OF AN ADVANCED SUBSYSTEM FOR THERMAL MANAGEMENT IN HYDROGEN-FUELED INJECTION VEHICLES. THE PROPOSED EFFORT WILL DETERMINE THE FEASIBILITY OF DEVELOPINGSUCH A COOLING SYSTEM USING NEW ALUMINA-SUPPORTED FORMULATIONS AS CATALYSTS FOR THE INTERCONVERSION OF PARA- AND ORTH ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  2. COMPUTER SIMULATION AND DESIGN OF JET NOISE SUPPRESSORS

    SBC: Aerochem Research            Topic: N/A

    COMPUTATIONAL, RATHER THAN EXPERIMENTAL, METHODS ARE PROPOSED TO DEVELOP, DESIGN, AND TEST THE NOISE SUPPRESSORS THAT WILL BE NEEDED TO QUIET THE JET TURBULENCE NOISE PRODUCED BY THE HIGH SPEED CIVIL TRANSPORT AND OTHER SUPERSONIC VEHICLES. THE VIABILITY OF THIS APPROACH IS DUE TO RECENT ADVANCES IN TURBULENCE THEORY AND NUMERICAL METHODS THAT COMBINE RENORMALIZATION GROUP METHODS AND SPECTRAL ELE ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  3. CROSS-CORRELATION OPTICAL STRAIN SENSOR FOR WIND TUNNEL TEST INSTRUMENTATION

    SBC: American Research Corporation of Virginia            Topic: N/A

    AEROSPACE STRUCTURES/MODELS ARE SUBJECTED TO HIGH TEMPERATURES AND STRONG AERODYNAMIC FORCES UNDER CAREFULLY CONTROLLED ENVIRONMENTAL CONDITIONS DURING INSTRUMENTED LABORATORY TESTING. WIND TUNNEL TESTING REQUIRES INSTRUMENTATION WHICH IS RUGGED, RELIABLE, ACCURATE AND PROVIDES TEST DATA QUICKLY TO THE TEST OPERATOR. MEASUREMENTS OF STATIC AND DYNAMIC STRAINS AND PROOF TESTING ON AEROSPACE STRUCTU ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  4. FLIGHT INSTRUMENTATION FOR SIMULTANEOUS DETECTION OF FLOW SEPARATION & TRANSITION

    SBC: ANALYTICAL SERVICES & MATERIALS INC            Topic: N/A

    A PORTABLE DATA ACQUISITION AND INSTRUMENTATION SYSTEM (DAISY) HAS BEEN DEVELOPED BY AS&M, INC. FOR WIND-TUNNEL TESTS. IT INCORPORATES A UNIQUE AND PATENTED TECHNIQUE TO ACCURATELY IDENTIFY AND DEMARCATE REGIONS OF FLOW SEPARATION, REATTACHMENT, AND THE LEADING-EDGE STAGNATION POINT. SIMULTANEOUSLY, LAMINAR-TO-TURBULENT TRANSITION AND THE SPECTRAL CONTENT OF THE MOST AMPLIFIED DISTURBANCES IN THE ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  5. FUEL CELL PROPULSION SYSTEM FOR A HIGH ALTITUDE RESEARCH PLATFORM

    SBC: AURORA FLIGHT SCIENCES CORPORATION            Topic: N/A

    THE INNOVATION PROPOSED FOR DEVELOPMENT IS A FUEL-CELL BASED ELECTRIC PROPULSION SYSTEM FOR VERY HIGH-ALTITUDE AIRCRAFT. THIS SYSTEM WOULD POTENTIALLY BE CAPABLE OF REACHING ALTITUDES OF UP TO 40 KM (131,000 FT) WITH A SCIENTIFIC PAYLOAD IN EXCESS OF 450 KG (1000 LBS). IT WOULDBE AN ATTRACTIVE PROPULSION ALTERNATIVE FOR NASA'S PROPOSED HIGH ALTITUDE RESEARCH PLATFORM (HARP) OR OTHER VERY HIGH ALTI ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  6. ROTOR UNSTEADY AIRLOADS

    SBC: CONTINUUM DYNAMICS INC            Topic: N/A

    OVER THE PAST SEVERAL YEARS, UNDER GOVERNMENT AND COMMERCIALSUPPORT, CONTINUUM DYNAMICS, INC. HAS MADE SIGNIFICANT PROGRESS IN COMPUTING THE UNSTEADY WAKES OF FIXED- AND ROTARY-WING AIRCRAFT. THIS PROGRESS, FOR THE MOST PART, RESULTED FROM THE SUCCESSFUL DEVELOPMENT OF THE BASIC CURVEDVORTEX ELEMENT AS A FUNDAMENTAL WAKE ELEMENT BUILDING BLOCK AND A NOVEL GENERALIZED VORTICITY CONTOUR REPRESENTATI ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  7. AEROACOUSTIC ANALYSIS OF ROTOR/ROTOR WAKE INTERACTIONS

    SBC: CONTINUUM DYNAMICS INC            Topic: N/A

    THE IMPORTANCE OF REDUCING THE NOISE EMITTED BY HELICOPTER ROTORS HAS BEEN WIDELY RECOGNIZED FOR MANY YEARS. PREVIOUS WORK BY CONTINUUM DYNAMICS IN THE ANALYSIS OF ROTOR AEROACOUSTICS LED TO THE DEVELOPMENT OF AN EFFICIENT AND ACCURATE LAGRANGIAN SIMULATION OF THE UNSTEADY VORTICITY FIELD IN THE VICINITY OF HELICOPTER MAIN ROTOR THAT COULD SERVE AS THE FOUNDATION FOR A GENERAL ANALYSIS OF THE NOIS ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  8. Sensor Fusion Software to aid in response and evacuation of subterranean incidents

    SBC: DAX TECHNOLOGIES INTERNATIONAL            Topic: HSB071002

    The speed at which an attack is detected is a critical trigger for all responses to follow. The accurate determination of the type of attack will determine the type of emergency personnel and response needed. The location will determine the target response area as well as determine by proximity which of the responders that are available can be first on the scene. Therefore, a system that can do th ...

    SBIR Phase II 2008 Department of Homeland Security
  9. WAVELENGTH DIPLEXED, FIBER COUPLED, COHERENT LASER RADAR MEASUREMENT SYSTEM

    SBC: DIGITAL SIGNAL CORP.            Topic: N/A

    THERE IS A NEED FOR FIBER COUPLED PROXIMITY SENSORS WITH HIGH SPEED AND ACCURACY FOR APPLICATIONS TO ROBOTIC END EFFECTORS AND TO AUTOMATED INSPECTION AND QUALITY CONTROL. THE PROPOSED PHASE I EFFORT WILL DEMONSTRATE A NOVEL, ROBUST, INTEGRATED SENSOR CONCEPT WITH MULTIPLE SENSOR CAPABILITY. FIBER OPTIC SENSORS HAVE BEEN DEMONSTRATED TO HAVE GEOMETRIC FLEXIBILITY. IN THE CASE OF PHASE MODULATED IN ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  10. "DEVELOPMENT OF A ROBUST NONEQUILIBRIUM PARABOLIZED NAVIER-STOKES CODE"

    SBC: Engineering Analysis Inc            Topic: N/A

    THE GOAL OF THIS RESEARCH IS TO PRODUCE A NEW, REAL GAS, THREE-DIMENSIONAL, PARABOLIZED NAVIER-STOKES (PNS) CODE WHICH IS MORE ROBUST, MORE ACCURATE, AND EASIER TO USE THAN THOSE PRESENTLY IN EXISTENCE. MOST "CURRENT DAY" PNS CODES (INCLUDING THE AFWAL PNS CODE) ARE BASED ON THE NONITERATIVE, IMPLICIT BEAM-WARMING FINITE-DIFFERENCE SCHEME. UNFORTUNATELY, CODES OF THIS TYPE HAVE PROVEN TO BEUNRELIA ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
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