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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. Synoptic approach to harmonize discrete data Streams in application development

    SBC: It Works Inc            Topic: 180NH1

    Synoptic approach to harmonize discrete data streams in application development 3/20/2018 Purchasing a new or used vehicle can be an exciting, but overwhelming experience. Numerous websites contain information on vehicle safety features, makes and models, cost, history, recalls, and crash and repair records. This large amount of data and its dispersed nature makes for a daunting consumer expe ...

    SBIR Phase I 2018 Department of Transportation
  2. Integrated Adaptive Route Capability

    SBC: CGH TECHNOLOGIES, INC.            Topic: A3

    This SBIR provides advanced, automated mechanisms for ANSPs and the flight operators to enrich and interact with IFR Preferred Routes in the U.S. National Airspace System (NAS). The FAA’s Instrument Flight Rules (IFR) Preferred Route Program was developed to allow air traffic facilities to identify select routes for use into and out of busy airports and airspace.  We apply automation to ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  3. A Decoupled Hydrogen Boost Electropumpfor Nuclear Thermal Propulsion

    SBC: T G V Rockets Inc            Topic: Z10

    NASA has identified Nuclear Thermal Propulsion (NTP) as an advanced propulsion concept for human missions to Mars.  It is seeking technologies related to NTP for development of the reactors and technologies needed for ground testing.  In the area of ground testing, NASA is interested in approaches to efficiently generate high temperature, high flow rate hydrogen.  TGV Rockets, Inc., ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  4. Integrated Powerhead for Methane Propulsion Systems

    SBC: T G V Rockets Inc            Topic: Z1002

    Development of an electric powerhead or Electropump for a 25,000 lb class Methane engine. Components for integrated RCS (~100-lb class) and Main Propulsion System (MPS) (25,000-lb class) feed systems (utilizing common propulsion tanks)"

    SBIR Phase I 2017 National Aeronautics and Space Administration
  5. 3D Polar Woven Deployable Skirt with Integrally Woven Attachment Features

    SBC: T.E.A.M., INC.            Topic: Z702

    T.E.A.M., Inc. proposes to develop and demonstrate a manufacturing method for a 3D woven deployable skirt structure with polar fiber orientation and integrally woven rib attachment features and trailing edge radii. The novelty of our approach comes from the combination of several unique textile manufacturing technologies that to our knowledge have never been successfully combined into a single pr ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  6. 3D Flow Field Measurements using Aerosol Correlation Velocimetry

    SBC: AeroMancer Technologies Corporation            Topic: A108

    AeroMancer Technologies proposes to develop a 3D Global Lidar Airspeed Sensor (3D-LGAS) using Aerosol Correlation Velocimetry for standoff sensing of high-resolution spatially and temporally resolved three-component global airspeeds using a scanning elastic lidar. The proposed instrument uses range-resolved elastic backscatter data from a scanning lidar beam to generate a 3D map of aerosol density ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  7. Ultrasonic Additive Manufacturing for High Performance Combustion Chambers

    SBC: T G V Rockets Inc            Topic: H201

    The objective of this proposal is to demonstrate the feasibility of using ultrasonic additive manufacturing (UAM) to dramatically reduce the cost and lead-time of fabricating rocket engine chambers, particularly high performance rocket engine chambers. Rocket engine combustion chambers require a very complex geometry, consisting of a cylinder of varying diameter, with a variable wall thickness, an ...

    SBIR Phase I 2016 National Aeronautics and Space Administration
  8. 3D Flow Field Measurements using Aerosol Correlation Velocimetry

    SBC: AeroMancer Technologies Corporation            Topic: A108

    AeroMancer Technology proposes to develop a 3D Lidar Global Airspeed Sensor (3D-GLAS) for remote optical sensing of three-component airspeeds in wind tunnel applications. Current methods of non-intrusive airspeed measurement include techniques such as Laser Doppler Velocimetry (LDV), Particle Imaging Velocimetry (PIV) and Doppler Global Velocimetry (DGV). However, some common drawbacks of all thes ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  9. Integration of Complex Geometry, 3D Woven Preforms via Innovative Stitching Technique

    SBC: T.E.A.M., INC.            Topic: H701

    Thick, 3D woven carbon/phenolic composites offer potential improvement over legacy thermal protection systems (TPS) for re-entry vehicle heat shield applications. However due to the scale and complexity of typical re-entry vehicle structures, it is likely that multiple 3D woven panels would need to laid up to create the overall heat shield, creating potential weak spots at the panel joints. In Pha ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  10. Integration of Complex Geometry, 3D Woven Preforms via Innovative Stitching Technique

    SBC: T.E.A.M., INC.            Topic: H701

    Thick, 3D woven carbon/phenolic composites offer potential improvement over legacy thermal protection systems (TPS) for re-entry vehicle heat shield applications. However due to the scale and complexity of typical re-entry vehicle structures, it is likely that multiple 3D woven panels would need to laid up to create the overall heat shield, creating a potential weak spots at the panel joints. ...

    SBIR Phase I 2014 National Aeronautics and Space Administration

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