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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

  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. Optimization of Supersonic Jet Noise Using a Reynolds-Averaged Navier-Stokes Approach

    SBC: SCIENTIFIC SIMULATIONS            Topic: A1

    The objective of this proposal is the development and demonstration of a cost-effective high-fidelity aeroacoustic design tool for future commercial supersonic nozzle designs and installations. Although eddy-resolving CFD methods for computing high-speed jet noise are available, such methods are computationally expensive and are currently deemed impractical for use in a design optimization loop. ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  3. 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 maintain ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  4. Integrated Launch Vehicle Booster using a Rocket Engine with a Combined Thermodynamic Cycle

    SBC: FRONTIER ASTRONAUTICS, LLC            Topic: Z9

    The concept describes a booster for a launch vehicle that is simpler to make, transport and launch than current launch vehicles. It is composed of two major components. The first being a booster structure and the second being a liquid rocket engine that uses a thermodynamic cycle that is a combination of two common cycles.Furthermore, the engine is actually fairly simple when compared to modern li ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  5. 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., proposes devel ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  6. 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 crossed polariz ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
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