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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. An Ontogenic Polynomial Neural Network/Expert System Modeling Evnironment for Chaotic Avionics Systems Behavior Prediction

    SBC: ABTECH CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  2. RECYCLING PROCESS FOR AIRCRAFT PLASTICS AND COMPOSITES

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

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  3. A NOVEL VERY-LOW-COST AIRBREATHING PROPULSION SYSTEM

    SBC: Adroit Systems, Inc.            Topic: N/A

    CURRENTLY, AIRBREATHING PROPULSION SYSTEMS WHICH OPERATE IN THE HIGH SUBSONIC REGIME ARE EXPENSIVE, COMPLEX, HEAVY AND USE PERISHABLE FUELS. TO OVERCOME THESE LIMITATIONS, A NOVEL PROPULSION CONCEPT BASED ON A PULSE DETONATION ENGINE (PDE) OR A CONVENTIONAL RAMJET COMBUSTOR (CRC) COUPLED WITH A BORON SOLID FUELED HYBRID GAS GENERATOR (HGG) IS PROPOSED. THE INNOVATION DRAWS FROM RECENT SUCCESSES IN ...

    SBIR Phase II 1993 Department of DefenseAir Force
  4. A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    This proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration into a new Combined Cycle Engine with Ramjets. The concept is an intermittent combustion jet engine that harnesses travelling detonation waves to accomplish compression and chemical reaction. The goal ...

    SBIR Phase I 1993 Department of DefenseAir Force
  5. A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    An innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereby reducing cooling requirements and aircraft weight while improving engine performance. Specifically, CONvective and TRANspiration cooling (CONTRAN) are uniquely combined, relying on hydrogen coolant ...

    SBIR Phase I 1993 Department of DefenseAir Force
  6. Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  7. Instrumentation for Non-Intrusive Water Droplet Size and Mass Flux Measurements Utilizing the Phase Doppler Method

    SBC: Aerometrics Inc.            Topic: N/A

    There is a need for non-intrusive instrumentation to characterize the drop size distribution and volume flux in support of on-line engine/inlet icing tests. The ducts may vary from three to twelve feet in diameter with flow field speeds from Mach 0.2 to 0.5. The Phase Doppler technique offers the best potential for making these measurements non-intrusively and with sufficient accuracy to meet the ...

    SBIR Phase I 1993 Department of DefenseAir Force
  8. Characterization of Simulated Weather Environments In Aerospace Ground Test Cells.

    SBC: Aerometrics Inc.            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  9. INCORPORATION OF ARBITRARY GRID PATCHING INTO GASP VERSION 3.0

    SBC: AEROSOFT INC            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  10. INFLATABLE SMART MISSILE WING DESIGN EVALUATION

    SBC: AEROTECH ENGINEERING & RESEARCH CORP.            Topic: N/A

    THREE AREAS OF ACTIVE MISSILE WING RESEARCH WILL BE PURSUED. THE FIRST SECTION WILL EVALUATE THE MATERIALS TO BE USED IN THE INFLATABLE WING SPARS, RIBS, SKINS, PRESSURE BLADDERS AND ACTIVE ELEMENTS. SPECIMENS OF HIGH ORTHOGONALITY COMPOSITES (POLYURETHANE-GRAPHITE) WILL BE CONSTRUCTED ALONG WITH SAMPLE ISOTROPIC BLADDER MATERIALS (MYLAR OR TEFLON) SO THAT THEIR FUNDAMENTAL PROPERTIES CAN BE EVALU ...

    SBIR Phase II 1993 Department of DefenseAir Force
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