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Award Data

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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. Torch-Augmented Spark Igniter for Nanosat Launch Vehicle LOX/Propylene Rocket Engine

    SBC: Garvey Spacecraft Corporation            Topic: T101

    The technical innovation proposed here is the introduction of torch-augmented spark ignition for high performance liquid oxygen (LOX) / propylene rocket engines now in development for a future two-stage nanosat launch vehicle. Spark ignition is critical for reliably achieving multiple in-flight restarts of NLV upper stage engines. In addition, this new capability will generate immediate R&D benef ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  2. 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
  3. Hybrid Modeling Capability for Aircraft Electrical Propulsion Systems

    SBC: PC KRAUSE & ASSOCIATES INC            Topic: T1501

    PC Krause and Associates is partnering with Purdue University, EleQuant, and GridQuant to create a hybrid modeling capability. The combination of PCKA?s extensive dynamic modeling experience, Purdue?s work in electromechanical systems analysis, and GridQuant and Elequant?s development of the HELM algorithm uniquely positions the team to create this technology. HELM is a novel algorithm that solves ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  4. Sustainable Water Purification

    SBC: STREAMLINE AUTOMATION LLC            Topic: T603

    Newly developed phase-engineered and low dimensional materials have opened the door to the design of materials structures that exhibit extremely efficient ionic transport. Recently, a new type of electro-filtration system designed to convert thermal power into purified water from salt water (or other ionic pollutants) has been demonstrated in the lab. The system is based on a bi-phasic nanoplate ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. 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
  8. 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
  9. 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
  10. Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design

    SBC: M4 ENGINEERING, INC.            Topic: T401

    We propose the development of a novel aerodynamic modeling approach making use of fully unstructured grids for unsteady panel aerodynamic models for aeroelastic and aeroservoelastic analysis. The unsteady aerodynamic code will be integrated with an existing suite of aeroelastic and aeroservoelastic analysis tools making it possible to perform aeroelastic and aeroservoelastic analysis of complex v ...

    STTR Phase II 2016 National Aeronautics and Space Administration
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