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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. Ultrasonic Additive Manufacturing of a deep throttling methane injector.

    SBC: T G V Rockets Inc            Topic: T9

    Design and manufacture of a Liquid fuel injector optimized for Ultrasonic Additive Manufacturing. UAM delivers aerospace parts today at 97% of bulk material property and foil laydown rates at speeds significantly better then powder or filament process. UAM has traditionally been applied to 2-D planar surfaces. We will extend UAM into complex geometries and constructs suitable for rocket engine inj ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  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. Low Cost Intermediate Stage for Affordable Nano/Micro Launch

    SBC: T G V Rockets Inc            Topic: T101

    NASA is extremely interested in developing small space launch capability. Small launchers are more sensitive to dry mass growth, more so then larger vehicles. Three stage launchers tend to be much more insensitive to Dry mass growth. The challenge then becomes how to meet strict cost targets when additional parts count increases. Use of Propane derived fuel helps reduce cost by allowing common b ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  6. Holomorphic Embedding for Loadflow Integration of Operational Thermal and Electric Reliable Procedural Systems

    SBC: EleQuant Knowledge Innovation Data Science LLC            Topic: T302

    This sound, low risk proposal aims at developing technology for the fundamental modeling and data processing needs of future autonomous operation. It addresses problems of early anomaly and fault detection in PMAD systems, adopting a larger scope by also including the thermal system. Truly autonomous operation of large power systems (e.g. ISS) cannot be scripted. In the quest to replace expert hum ...

    STTR Phase I 2017 National Aeronautics and Space Administration

    SBC: Narf Industries LLC            Topic: HSB0161002

    Existing blockchain implementations do not include features required for an effective, decentralized and scalable identity management solution. Although current public (permissionless) blockchains provide rigorous, self-incentivizing primitives to ensure the integrity, availability, and non-repudiation of events, they often intentionally eschew confidentiality features as anathema to the consensu ...

    SBIR Phase I 2016 Department of Homeland Security
  8. 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
  9. Low Cost Upper Stage for Affordable Nano/Micro Launch

    SBC: T G V Rockets Inc            Topic: T101

    TGV Rockets, Inc., in partnership with the University of Tennessee, Knoxville, proposes to develop a unique Low-Cost Upper Stage for Affordable Nano/Micro Launch. The stage will make use of a novel eutectic fuel blend that is thermally compatible with liquid-oxygen, unique low-cost lightweight avionics, and simple common-wall tanks. The projected production cost of the completed upper stage is a ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  10. 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

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