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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. Arrays of Remote Autonomous Sensors Using On-Board Hybrid Power Supplies

    SBC: BIPOLAR TECHNOLOGIES            Topic: F307

    There is significant need for arrays of miniature sensors that are completely wireless. Ideally these sensors would be built as an integrated device, including sensing elements, computation/signal conditioning, communication, and an on-board power supply. However, they have not been developed due to the difficulty with integrating sensing ele-ments, and the absence of miniature power supplies. ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  2. Co-Generation of High Purity Hydrogen and Electric Power

    SBC: Technology Holding, LLC            Topic: A202

    The proposed innovation is an integrated hybrid solid state electrochemical system providing co-generation of high purity hydrogen and electric power. The embodiment is a physical, chemical and thermal integration of three processes: (1) production high purity hydrogen, (2) electrochemical partial oxidation of hydrocarbon fuel, and (3) power generation by a solid oxide fuel cell. This highly integ ...

    SBIR Phase II 2004 National Aeronautics and Space Administration
  3. High Temperature Solid State Lithium Battery

    SBC: Technology Holding, LLC            Topic: S402

    Reliable energy systems with high energy density capable of operating at high temperatures, pressures and radiation levels are needed for certain NASA missions. Batteries based on solid-state ceramic oxide composite electrolytes provide the benefit of operation at temperatures up to 550o C. The current high-temperature Li battery technologies use carbonate, chloride and other molten compounds bas ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  4. Emissive Ion Thruster-EMIT

    SBC: Technology Holding, LLC            Topic: S102

    A propulsion system is proposed that is based on acceleration of ions emitted from a thin, solid-state electrochemical ceramic membrane. This technology would provide a versatile propulsion system that would be suitable for long-term, low-thrust missions throughout the deep-space to near-Earth range. The specially formulated and fabricated membrane in combination with an applied bias voltage wil ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  5. The cryogenic evaluation of typical and experimental filament winding materials

    SBC: Hypercomp Engineering, Inc            Topic: H306

    HyPerComp Engineering, Inc. (HEI) proposes to develop well characterized, reliable filament wound composite pressure vessels for cryogenic and other low temperature applications. The proposed effort also explores the potential for a significant improvement in filament wound composite pressure vessels performance (end results: lighter weights) through cryogenic process treatment. Both the aerospac ...

    SBIR Phase II 2004 National Aeronautics and Space Administration
  6. SSVD Extreme Temperature Electronics for Planned Venus Missions

    SBC: INNOSYS, INC.            Topic: S402

    The purpose of this project is to demonstrate, based on a new class of electronic devices called solid state vacuum devices (SSVD?s), a highly promising enabling technology for extreme high temperature radiation hard electronics. SSVD?s marry solid state semiconductor technology, including the process fabrication techniques, with vacuum electronics, and, in this case, specifically thermionic vacu ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  7. Ultraviolet AlGaN-based Avalanche Photo Diode Grown over Single Crystal Bulk AlN Substrates

    SBC: Sensor Electronic Technology, Inc.            Topic: E101

    Premature breakdown is a key obstacle in developing AlGaN-based avalanche photo diodes (APD) for ultraviolet (UV) light detection. Novel materials growth techniques, such as Hydride Vapor Phase Epitaxy (HVPE) allows for reduction of dislocation density only to approximately 10^7 cm-2. In order to reduce the number of growth defects and dislocation density in AlGaN-based APDs we will use single cry ...

    SBIR Phase I 2004 National Aeronautics and Space Administration

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