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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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. Modular Embedded Intelligent Sensor Network

    SBC: Angstrom Designs, Inc.            Topic: T1301

    Remote sensing, when combined with real-time processing, provides instant feedback on safety, mission success and system health. Being able to combine embedded sensing with distributed networks gives us the additional potential to further benefit many systems and sub-systems in the aerospace industry including launch vehicles, ground test equipment and spacecraft. These remote distributed sensor ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  2. Low Mass/Power Sensor Suite for Spacesuits

    SBC: SEACOAST SCIENCE, INC.            Topic: T601

    To provide additional telemetry and data for long-term mission, the composition of internal atmosphere of spacesuits must be determined. Specifically, the unambiguous detection and quantification of carbon dioxide is crucial for mission completion. Detection of other gasses (ammonia, oxygen) is also necessary for a complete sensor suite. Seacoast Science and Case Western Reserve University pro ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  3. Sensitivity Analysis for Design Optimization Integrated Software Tools

    SBC: Linked, Inc.            Topic: T401

    The objective of this proposed project is to provide a new set of sensitivity analysis theory and codes, the Sensitivity Analysis for Design Optimization Integrated Software Tool set, to work within the existing NASA O3 Tool. In this Phase I effort, the sensitivity approach will be implemented for two basic types of analysis, namely static systems of equations (linear and non-linear) and eigen-pro ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  4. Robotic ISRU Construction of Planetary Landing and Launch Pad

    SBC: Honeybee Robotics, Ltd.            Topic: T402

    The Apollo 15 Lunar Module rocket plume excavated regolith which sandblasted at speeds in excess of 1000 m/s the Surveyor 2 lander 200 m away. A Curiosity rover instrument was permanently damaged during SkyCrane landing on Mars. Any future human surface missions to planetary bodies covered in regolith (e.g. Mars, Moon) would need to address ejecta created during landing or takeoff. The intent of ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  5. An Additive Manufacturing Technique for the Production of Electronic Circuits

    SBC: Morningbird Media Corporation            Topic: T1204

    The proposed 9-month research project aims for the development of additive manufacturing techniques for the creation of electronic devices. It will develop an innovative additive manufacturing technique that combines the ink-based printing with laser melting technology to directly print a three-dimensional (3D) system with built-in electrical properties and functioning as an electronic device. Th ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  6. In-Situ Spectroscopic Europa Explorer (ISEE)

    SBC: Honeybee Robotics, Ltd.            Topic: T803

    The US congress has instructed NASA to include a lander component in the next Europa mission. The mission has a target launch date of 2022, and its primary goal will be to search Europa?s icy surface for evidence of life that may persist within the ice shell or subsurface ocean. The Europa lander study specifically recommends a combination of a mass spectrometer and a Raman spectrometer to investi ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  7. Robotic Tool for Asteroid Resource Prospecting and Characterization

    SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP            Topic: T402

    Optical fibers are inherently tolerant of cosmic radiation and a wide temperature range, immune to electromagnetic noise and thus solar flares, etc. Embedded fiber sensors can be highly resistant to shock and vibration, hence their usage in the oil drilling industry. IFOS will work with Stanford?s Center for Design Research to develop a robotic prospecting tool with fiber-optic based haptic sensi ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  8. Structural Nervous System

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T1201

    GTL?s SNS technology aids in the operation of new or existing structural health monitoring (SHM) systems by integrating data and power pathways into the structure. The use of this technology within a composite structure would allow engineers to place sensors from an SHM system directly where they are needed on a structure with instant power. GTL?s SNS technology offers the potential for developers ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  9. Active Radiation Shield

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T301

    DEC-Shield technology offers the means to generate electric power from cosmic radiation sources and fuse dissimilar systems and functionality into a structural component to create a Multi-functional Structure (MFS). DEC-Shield integrated into MFS technology can be used to generate electric power and provide radiation protection in a space vehicle; even maximizing that protection by spreading the ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  10. Prediction of Strutural Response and Fluid-Induced Vibration in Turbomachinery

    SBC: CFD RESEARCH CORPORATION            Topic: T102

    Advanced turbomachinery components play a critical role in launch vehicle and spacecraft liquid rocket propulsion systems. To achieve desired efficiencies, extremely tight tolerances are often imposed between inducer blades and shrouds or other system components which sets up strong interactions that influence both the aerodynamics and the structural performance of blades and vanes. These transien ...

    STTR Phase I 2016 National Aeronautics and Space Administration
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