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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. Extremely High Suction Performance Inducers for Space Propulsion

    SBC: Concepts NREC, LLC            Topic: T901

    Advanced pump inducer design technology that uses high inlet diffusion blades, operates at a very low flow coefficient, and employs a cavitation control and stability device. A preliminary scoping inducer test with this technology indicated a doubling of the suction specific speed capability over current inducers. A three to four fold increase over current technology is the goal of this research ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  2. High Power High Thrust Ion Thruster (HPHTion): 50 CM Ion Thruster for Near-Earth Applications

    SBC: Electrodynamic Applications Inc            Topic: T301

    Advances in high power, photovoltaic technology has enabled the possibility of reasonably sized, high specific power, high power, solar arrays. New thin film solar arrays have demonstrated specific powers of over 4000 W/kg (exceeding the current SOA of ~130 W/kg). At high specific powers, power levels ranging from 50 to several hundred kW are feasible for communication satellites. Coupled with ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  3. Innovative Solid State Lighting Replacements for Industrial and Test Facility Locations

    SBC: Energy Focus, Inc.            Topic: T1002

    The proposed innovation is the replacement of existing test stand and parking lot fixtures with current SSL LED technology. The replacement fixtures will reduce energy consumption, generate less heat and provide maintenance free operation for over 50,000 hours. An explosion-proof fixture is capable of containing an internal combustion event without allowing flames or hot gasses to escape to the s ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  4. Magnetically Modified Asymmetric Supercapacitors

    SBC: GINER INC            Topic: T601

    This Small Business Innovation Research Phase I project is for the development of an asymmetric supercapacitor that will have improved energy density and cycle life. Supercapacitors that utilize an aqueous electrolyte are limited to a maximum voltage of 1 volt due to the decomposition of water. Methods used to increase voltage include use of an organic electrolyte, which introduces additional comp ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  5. Time-Domain Terahertz Reflection Holograhic Tomography Nondestructive Evaluation System

    SBC: TeraMetrix, LLC            Topic: T701

    We propose to demonstrate key elements of feasibility for a single-sided time-domain terahertz reflection holographic tomographic imaging (TD-THz RHT) nondestructive evaluation (NDE) system which will provide high quality three dimensional images of the interior of complex aerospace composite structures. Time-domain terahertz imaging in the 0.1 to 3 THz spectral range is currently being used to c ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  6. Gaseous Helium Reclamation at Rocket Test Systems

    SBC: Sierra Lobo, Inc.            Topic: T1001

    The ability to restore large amounts of vented gaseous helium (GHe) at rocket test sites preserves the GHe and reduces operating cost. The used GHe is vented into the atmosphere, is non-recoverable, and costs NASA millions dollars per year. Helium, which is non-renewable and irreplaceable once released into the atmosphere, is continuously consumed by rocket test facilities at NASA centers such a ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  7. Next-Generation Ion Thruster Design Tool to Support Future Space Missions

    SBC: TECH-X CORPORATION            Topic: T301

    Computational tools that accurately predict the performance of electric propulsion devices are highly desirable by NASA and the broader electric propulsion community. Large investments in running the long duration test programs (> 20 kHrs) at NASA GRC can be reduced with computer models and allow more focus on exploring the NEXT ion thruster design for future space missions. The current state of e ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  8. Terahertz Quantum Cascade Laser Based 3D Imaging

    SBC: LONGWAVE PHOTONICS LLC            Topic: T7

    The NASA Constellation program has a need to non-destructively test (NDT) non-metallic materials (foams, Shuttle Tile, Avcoat, etc) for defects such as delaminations and voids. While imaging systems at terahertz frequencies (0.3 to 3 THz) have been demonstrated for 2D imaging of similar materials, they have not yet demonstrate full 3D volumetric imaging. To meet this need, LongWave Photonics pro ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  9. Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems

    SBC: STREAMLINE NUMERICS, INC.            Topic: T901

    The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a pr ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  10. OrFPGA: An Empirical Performance Tuning Tool for FPGA Designs

    SBC: RNET TECHNOLOGIES INC            Topic: T1101

    With the capacity and performance of FPGAs suitable for space borne applications continuously increasing, the design of FPGAs is becoming increasingly complex involving trading off or simultaneous optimization of space, speed, and power. RNET and ANL are proposing to develop software infrastructure that facilitates automatic performance tuning of FPGAs in terms of speed, power, and size. We introd ...

    STTR Phase I 2013 National Aeronautics and Space Administration
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