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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. Optical Line Filter and Spectrometer based Upon Two-Photon Absorption for Doppler LIDAR at 1.053 um

    SBC: ESPYLUX LLC            Topic: S1

    A receiver system for use in LIDAR consisting of an optical filter and optical spectrometer based upon two-photon absorption is proposed.  The filter and spectrometer both use dispersion from excited state transitions of atomic rubidium  to create a birefringent medium. The birefringent medium of the optical filter rotates the polarization of light so that it is transmitted through cross ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. 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
  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. Fail-Safe, Controllable Liquid Spring/Damper System for Improved Rover Space Vehicle Mobility

    SBC: Advanced Materials and Devices            Topic: H601

    NASA is planning to return to the moon in 2020 to explore thousands of miles of the moon?s surface with individual missions, lasting six months or longer. Surface mobility is critical to outpost buildup and exploration activities, where the change in the vehicle weight between unloaded and loaded cargo conditions and travel over rough terrain can adversely affect the ride handling conditions and ...

    SBIR Phase I 2016 National Aeronautics and Space Administration
  10. 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

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