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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. QMU in Integrated Spacecraft System Models

    SBC: ACTA, LLC            Topic: T5

    ACTA and Sandia National Laboratories propose to quantify and propagate substructure modeling uncertainty for reduced-order substructure models to higher levels of system assembly, thereby enabling predictive simulations of engineering designs with quantified margins and uncertainties for model-based flight qualification of complete spacecraft. A critical part of this process is the accurate mode ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  2. Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization

    SBC: AMERICAN GNC CORPORATION            Topic: T1

    In providing an innovative solution to improving information technologies and health management systems, AGNC is proposing a significant technological achievement with the Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization. During in-flight conditions, this system is able to not only provide the status of information such as regarding the flight envel ...

    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. Biotemplated Nano-Structured Materials for Advanced Li-ion Batteries

    SBC: CFX BATTERY, INC.            Topic: T301

    NASA has identified a critical need for pioneering advances in battery technology to give high performance, low-weight, durable and long-life power sources for future missions. In this Phase I proposal, CFX Battery, Inc. and Georgia Institute of Technology propose the chemical conversion of micron-sized, nano-structured templates available from renewable resources into functional electrode materia ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  5. Advanced Li/CFx Primary Batteries with Non-Flammable Electrolytes

    SBC: CFX BATTERY, INC.            Topic: T601

    NASA seeks to develop high specific energy primary batteries that are safe and capable of performing under a wide temperature range, for manned space missions. To meet this goal, CFX Battery Inc. proposes to develop, characterize, and establish technological feasibility of a new Li/SF-CFx based high capacity lithium primary battery that offers higher rate capability and enhanced safety than conven ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  6. Highly Reliable Structural Health Monitoring of Smart Composite Vanes for Jet Engine

    SBC: Intelligent Fiber Optic Systems Corporation            Topic: T201

    Intelligent Fiber Optic Systems and Auburn University propose a Fiber Bragg Grating (FBG) integrated Structural Health Monitoring (SHM) sensor system capable of providing in-situ crack detection, location and quantification of damage, as well as validating structural models, using recent advances in non-contact, non-destructive dynamic testing of composite structures. The key innovation is an FBG- ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  7. 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
  8. Quantification of Uncertainties in Integrated Spacecraft System Models

    SBC: M4 ENGINEERING, INC.            Topic: T501

    The proposed effort is to investigate a novel uncertainty quantification (UQ) approach based on non-intrusive polynomial chaos (NIPC) for computationally efficient and accurate quantification of uncertainties in spacecraft system models within a multidisciplinary analysis and optimization (MAO) framework. The UQ approach will include the modeling of both inherent (probabilistic) and epistemic unc ...

    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. 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
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