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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. UV Rigid Inflatable Wing

    SBC: Adherent Technologies, Inc.            Topic: N/A

    As the unmanned exploration of Mars and Venus becomes more of a focus area at NASA, inflatable, rigidizable wings will become an enabling technology. The successful development of this type of wing will also have significant military applications. The utility of unmanned aerial vehicles (UAVs) for the military has been dramatically demonstrated in the conflict in Afghanistan. Rigidization of infla ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  2. HIGH-TEMPERATURE FINISH FOR AMB-21 MATRIX COMPOSITES

    SBC: Adherent Technologies, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration
  3. Novel Adhesives For Space Applications

    SBC: Adherent Technologies, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  4. SOFT HUB FOR BEARINGLESS ROTORS

    SBC: Advanced Technologies, Inc            Topic: N/A

    THE ROTARY WING INDUSTRY HAS STRIVED TO DEVELOP A BEARINGLESS MAIN ROTOR (BMR), HAVING NO MECHANICAL BEARINGS. ALL TRUE BMR SYSTEMS ARE LIMITED BY THE STRENGTH IN STATIC-FATIGUE LOADS VERSUS FLAPWISE FLEXIBILITY, RESULTING IN LIMITED "G" MANEUVERS FROM A HIGHLY RESPONSIVE ROTOR SYSTEM. ATI'S SOFT HUB ROTOR CONCEPT ALLOWS TILTING OF THE ROTOR DISC MOVING THE VIRTUAL HINGE INBOARD ELIMINATING THIS U ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  5. Autonomous Spacecraft Power Scheduling

    SBC: AEROASTRO, INC.            Topic: N/A

    AeroAstro and the University of Colorado propose to develop an autonomous satellite power control system to dynamically monitor, schedule and distribute power resources on microsatellites , while remaining sensitive to the mission objectives. The Autonomous Power Scheduler (APS) will maximize power efficiency and availability while being situationally-aware of bus conditions. The concept system wo ...

    STTR Phase I 2003 National Aeronautics and Space Administration
  6. MEMS Propulsion Technology Utilizing Decomposing Nitrous Oxide Propellant

    SBC: AEROASTRO, INC.            Topic: N/A

    A low cost, high performance propulsion system does not exist that can support small and micro-satellite requirements, that is not burdened with severe hazard and toxicity issues. The VACCO Micro Propulsion System (MPS) represents a leap forward in the application of ChEMS? (metal MEMS) propulsion technology for nanosat and picosat missions, however its capability is limited by reliance on low-Isp ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  7. Active Skin for Turbulent Drag Reduction

    SBC: AEROPROBE CORPORATION            Topic: N/A

    Drag reduction for aerial vehicles has a range of positive ramifications: reduced fuel consumption with the associated economic and environmental consequences, larger flight range and endurance and higher achievable flight speeds. Recent numerical results yielded solid evidence that very small disturbances in the form of a spanwise traveling force wave on a surface could reduce drag by 70%. Our pa ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  8. Seven-Sensor Probes For Dusty And/Or Compressible Flows

    SBC: AEROPROBE CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  9. A Stand-Alone Sensitivity Solver For Hypersonic Design Applications

    SBC: AEROSOFT INC            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  10. LASER SPECKLE INTERFEROMETER FOR SURFACE ACOUSTIC DISPLACEMENT MEASUREMENTS

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

    ADVANCES IN REAL-TIME MEASUREMENT TECHNIQUES FOR CHARACTERIZING STRUCTURAL AND PROPULSION SYSTEM PROPERTIES REQUIRE ACCURATE MEASUREMENT OF DYNAMIC PROPERTIES IMPORTANTTO THE DESIGN OF ADVANCED AERONAUTICAL AND AEROSPACE VECHICLES. THE SPECIFIC INNOVATION ADDRESSED BY THIS PROPOSAL IS THE EMPLOYMENT OF A NON-INTRUSIVE, RUGGED OPTICAL IMAGING METHOD COMPATIBLE WITH ROUGH AND POORLY REFLECTING ADVAN ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
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