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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. Acoustic Reduction of Flow Separation

    SBC: LYNNTECH INC.            Topic: T201

    Airfoils produce more lift and less drag when the boundary layer is attached to the airfoil. With most aircraft there are combinations of airspeed and angle of attack where the boundary layer at least partially detaches from the airfoil. Reducing boundary layer detachment will increase lift and reduce drag. This will reduce fuel consumption saving money for the operator and improving control fo ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  2. Active Electromechanical Suspension System for Planetary Rovers

    SBC: BALCONES TECHNOLOGIES LLC            Topic: T102

    Balcones Technologies, LLC proposes to adapt actively controlled suspension technology developed by The University of Texas at Austin Center for Electromechanics (CEM) for high performance off-road vehicles to address STTR 2009-1 Subtopic T1.02, Information Technologies for Intelligent Planetary Robots. In particular, our team will develop a concept design for an actively controlled ElectroMechan ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  3. Active Vibration Isolation System for Mobile Launch Platform Ground Support Equipment

    SBC: BALCONES TECHNOLOGIES LLC            Topic: T6

    During our Phase I STTR effort, Balcones Technologies, LLC and The University of Texas Center for Electromechanics (CEM) successfully achieved all Phase I objectives and developed a concept design for an active Vibration Isolation System (VIS) that fully meets all requirements defined or implied in STTR 2007-1 Subtopic T6.02. Now the Balcones Technologies - CEM team proposes to develop, test, and ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  4. A Cubesat Hyperspectral Imager

    SBC: NANOHMICS INC            Topic: T801

    Mapping spectrometers have been extremely useful in multiple NASA applications, from Earth composition mapping to identifying hydrocarbon lakes on Titan. Traditionally, imaging spectroscopy systems are not only heavy but also large in order to accommodate the long path lengths needed for spectral separation. There are several varieties, such as push-broom and scanning imaging spectrometers, but h ...

    STTR Phase II 2017 National Aeronautics and Space Administration
  5. Additive Manufacture of Refractory Metal Propulsion Components

    SBC: GEOPLASMA LLC            Topic: T9

    Niobium alloy (C-103) reaction control system (RCS) chambers have been used on numerous NASA programs. However at elevated temperatures, the strength of C-103 decreases significantly. Higher strength niobium alloys have been developed, but these alloys lack the formability of C-103. Recently, Additive Manufacture (AM) of niobium and C-103 has been demonstrated using powder bed electron beam me ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  6. Advanced Morphing Moulage for Medical Training (AMM-MT)

    SBC: VCOM3D INC            Topic: DHA17A002

    For this Phase I SBIR proposal, Vcom3D proposes to design advanced medical moulage that accurately simulates the progression of an injury or pathology by morphing through a series of clinical states to enable learners to confirm the progression of the wound and to determine whether iatrogenic errors or pathologies occurred duing treatment. The physical morphing moulage may be applied to medical m ...

    STTR Phase I 2017 Department of DefenseDefense Health Agency
  7. Advanced Simulation Framework for Design and Analysis of Space Propulsion Systems

    SBC: STREAMLINE NUMERICS, INC.            Topic: T901

    The innovation proposed here is a high-performance, high-fidelity framework in the computational fluid dynamics (CFD) code called Loci-STREAM to enable accurate, fast and robust simulations of unsteady multiphase flows such as combustion involving liquid-gas phases in liquid rocket injectors and solid-gas phases in solid rocket motors, and cryogenic cavitation in delivery systems of liquid rocket ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  8. Advanced Structural Health Monitoring

    SBC: TEXAS RESEARCH INSTITUTE , AUSTIN, INC.            Topic: T1201

    Frequency selective surfaces (FSSs) are periodic arrays of conductive elements or patches that cause a particular reflection or transmission response when illuminated with high frequency electromagnetic energy. These arrays have been used as high frequency filters and in radar, stealth and advanced antenna applications, and more recently, as sensors. In particular, FSS-based sensing has found a ho ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  9. Advanced Structural Health Monitoring

    SBC: TEXAS RESEARCH INSTITUTE , AUSTIN, INC.            Topic: T12

    Frequency selective surfaces (FSSs) are periodic arrays of conductive elements/patches that cause a particular reflection response when illuminated with high frequency electromagnetic energy. nbsp;These arrays arenbsp;used for high frequency filters and in antenna applications.nbsp; We propose to use FSSs as multi-functional sensors. nbsp;FSS sensors are unpowered, low-profile (thin), wireless and ...

    STTR Phase II 2019 National Aeronautics and Space Administration
  10. 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
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