You are here

Award Data

For best search results, use the search terms first and then apply the filters
Reset

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. REDUCTION OF SUPERSONIC PLUME NOISE THROUGH THE CONTROLLED INTRODUCTION OF AZIAL VORTICITY

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

    N/A

    SBIR Phase I 1992 National Aeronautics and Space Administration
  3. SUPERSONIC COMBUSTION ENHANCEMENT BY A NONEQUILIBRIUM PLASMA JET

    SBC: Aerochem Research            Topic: N/A

    IT IS PROPOSED TO DETERMINE THE FEASIBILITY OF USING A NONEQUILIBRIUM PLASMA JET, DEVELOPED AT AEROCHEM OVER THE PAST QUARTER CENTURY, AS A MEANS OF ENHANCING IGNITION AND FLAME STABILIZATION IN AIR-BREATHING ENGINES AND IN SUPERSONIC COMBUSTION. SPECIFICALLY, WE WILL DETERMINE; IF IGNITION OF LEAN OR LOW PRESSURE MIXTURES CAN BE MADE MORE RELIABLE; IF FLAME HOLDING LIMITS CAN BE BROADENED, E.G., ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  4. DIRECT COMPUTATION OF TURBULENCE NOISE

    SBC: Aerochem Research            Topic: N/A

    DIRECT COMPUTATION OF TURBULENCE NOISE IS A LOGICAL APPLICATION FOR ADVANCED COMPUTATIONAL FLUID DYNAMICS, CFD, PROGRAMS RUN ON SUPERCOMPUTERS. THIS WOULD ELIMINATE THE HIGHLY EMPIRICAL ASPECTS OF PRESENT NOISE PREDICTION TECHNIQUES AND ENABLE STUDY OF ADVANCED HYPERSONIC PROPULSION SYSTEMS. HOWEVER, MANY OF THE SAME PERSISTENT PROBLEMS OF IMPLEMENTATION THAT EXIST IN AEROACOUSTIC THEORY AND MEASU ...

    SBIR Phase II 1989 National Aeronautics and Space Administration
  5. GENERIC ARTIFICIAL INTELLIGENCE EXPERT SYSTEM FOR SPACE STATION APPLICATIONS

    SBC: Applications Resources Inc            Topic: N/A

    THE GENERIC ARTIFICIAL INTELLIGENCE EXPERT SYSTEM FOR SPACE-STATION APPLICATIONS WILL BE USER-FRIENDLY AND WILL UTILIZE A HIERARCHY OF FRAMES FOR DATA INPUT, AUTOMATIC FAULT DIAGNOSIS AND ANALYSIS AND REPAIR FUNCTIONS. IT WILL PROVIDE PROMPT DIAGNOSIS AND SUGGESTIONS FOR SYSTEM REPAIR. IT WILL PROVIDE AS MUCH AUTOMATION AS POSSIBLE FOR REPAIR FUNCTIONS. THE DESIGN WILL BE APPROPRIATE FOR INTERFACI ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  6. Emerging Weapons Technology Evaluation Model

    SBC: APPLIED SCIENCES LABORATORY, INC.            Topic: N/A

    Accelerated development of directed energy technologies has presented new problems to mission planners and weapon operators regarding the capabilities, lethality and performance of weapon systems. The Emerging Weapons Technology Evaluation Model willaddress these shortcomings by providing users of varying technical expertise 1) the ability to model a variety of weapons in various mission scenario ...

    SBIR Phase I 2003 Department of DefenseSpecial Operations Command
  7. DAMPER- DIGITAL ACTIVE MATERIALS-PROCESSING PLATFORM EFFORT

    SBC: A-TECH CORPORATION            Topic: N/A

    THE DIGITAL ACTIVE MATERIALS-PROCESSING PLATFORM EFFORT BE- ING PROPOSED HERE SEEKS TO DEVELOP AN ACTIVELY STABILIZD PLATFORM UPON WHICH MICRO-G MATERIALS PROCESSING EXPERIMENTSCAN BE PERFORMED IN SPACE. WITH THE SUC- CESSFUL COMPLETION OF THE TWO-STEP PHASE I WORKPLAN APPLIED TECHNOLOGY ASSOCIATES (ATA) HAS CLEARLY AND SUCCINTLY DEFINED THE PROBLEM OF PLATFORM ISOLATION IN SPACE AND HAS COMPLETEL ...

    SBIR Phase II 1989 National Aeronautics and Space Administration
  8. Intelligent Variable Emittance Panels Using New, ""True"" Solid Electrolyte

    SBC: Ashwin-Ushas Corporation            Topic: N/A

    This firm has, in ongoing work in collaboration with the Air Force, NASA and JPL, developed a unique Variable Emittance technology based on the electrochromism of unique Conducting Polymers. This comprises thin (< 0.5 mm), flexible, lightweight (0.16 g/cm^2), variable area (0.5 cm^2 to 0.5 m^2), very low cost flat panels. Delta Emittance (DE) of 0.33 in space-qualified devices, and 0.53 in vacuum- ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  9. ADVANCED TURBOMACHINERY CFD DESIGN AND ANALYSIS PROGRAM

    SBC: Cambridge Hydrodyn Inc            Topic: N/A

    COMPUTATIONAL FLUID DYNAMICS (CFD) TOOLS HAVE NOW DEVELOPED TO THE POINT WHERE THEY CAN BE RELIABLY USED FOR THE DESIGN,EVALUATION, AND ANALYSIS OF SUCH HIGH-PERFORMANCE GAS TURBINES AS THOSE USED IN MODERN AERONAUTICAL PROPULSION SYSTEMS. FOR THESE APPLICATIONS, IT IS NECESSARY TO USE A THREE-DIMENSIONAL VISCOUS CFD CODE THAT COMBINES EFFICIENCY,ACCURACY, AND USER-FRIENDLINESS. FOR AXIAL TURBOMAC ...

    SBIR Phase II 1992 National Aeronautics and Space Administration
  10. A MATHEMATICALLY BASED REYNOLDS-STRESS MODEL OF TURBULENCE

    SBC: Cambridge Hydrodyn Inc            Topic: N/A

    N/A

    SBIR Phase I 1992 National Aeronautics and Space Administration
US Flag An Official Website of the United States Government