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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY21 is not expected to be complete until September, 2022.

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.

  1. 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
  2. Three-Dimensional Backscatter X-Ray Imaging System

    SBC: ARIBEX            Topic: T7

    The overall objective of the proposal is to design, develop and demonstrate a potentially portable Compton x-ray scatter 3D-imaging system by using specially designed rotationally movable x-ray source and x-ray detector, and the development of a suitable 3D-processing computer model. The proposed rotational configuration will allow the acquisition of multiple projections or images 360

    STTR Phase I 2010 National Aeronautics and Space Administration
  3. 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
  4. 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
  5. 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
  6. 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
  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. Integration of Notification with 3D Visualization of Rover Operations

    SBC: Traclabs Inc.            Topic: T102

    3D visualization has proven effective at orienting remote ground controllers about robots operating on a planetary surface. Using such displays, controllers can watch a robot move through surface terrain maps and react to objects in that terrain. Readings taken in the robot's surroundings can be overlaid on terrain maps to improve human understanding. 3D visualization, however, focuses a contro ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  9. Distributed Diagnosis, Prognosis and Recovery for Complex Systems

    SBC: Traclabs Inc.            Topic: T101

    Complex space systems such as lunar habitats generate huge amounts of data. For example, the International Space Station (ISS) has over 250,000 individually identified pieces of low-level telemetry and commands. Innovative algorithms for collecting and analyzing this data are leading to new technologies for managing large, complex and distributed systems. Lunar habitats will have multiple inte ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  10. 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
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