Award Data

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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 June, 2020.

  1. 355 nm Laser Design for Atmospheric Measurements

    SBC: Cutting Edge Optronics, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration
  2. Tri-Spectroscopy Interferometric Micro-imaging Sensor

    SBC: MEDECO, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration
  3. 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-resolvingnbsp; 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 lo ...

    SBIR Phase II 2019 National Aeronautics and Space Administration
  4. A Next Generation Spacecraft Heat Rejection System

    SBC: Thermavant Technologies, L.L.C.            Topic: Z2

    In response to NASA SBIR FY 2018 topic Z2.01, Thermal Management, ThermAvant Technologies, LLC proposes to develop an innovative, passive heat transfer device that can significantly improve the spacecraft#39;s thermal control system, namely around heat acquisition and rejection capabilities.nbsp; ThermAvant proposes to develop an advanced Oscillating Heat Pipe (OHP) based heat rejection system tha ...

    SBIR Phase II 2019 National Aeronautics and Space Administration
  5. Development of A Digital Assistant for Early Mission Analysis and Design

    SBC: MYCROFT AI INC            Topic: T11

    The objective of this Phase I STTR proposal is to develop a first prototype of a digital assistant to support NASA engineers in space mission engineering and design tasks in Pre-Phase A and Phase A mission studies. This technology will: 1) increase the quality and diversity of the designs explored during early stage mission concept studies; 2) decrease the time and resources it takes to perform su ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  6. DiSCO: Dual In-Situ Spectroscopy and Coring

    SBC: Impossible Sensing            Topic: S1

    We propose an innovative arm-mounted instrument for acquiring and analyzing planetary subsurface materials. The instrument extracts 5times;1cm cores, and immediately performs in-situ, time-resolved, coregistered imaging and spectroscopic mapping at high resolution ndash; 10micro;m and 50micro;m, respectively. Rapid analysis of cores is critical to characterize original material before it has time ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
  7. A Multifunctional Hypersonic Leading Edge with Integrated Thermal Management

    SBC: Thermavant Technologies, L.L.C.            Topic: A1

    In response to NASA SBIR FY 2018 topic A1.10, Hypersonic Technology, ThermAvant Technologies, LLC (ThermAvant) proposes to develop a high temperature, conformal thermal-mechanical leading edge skin for hypersonic aircraft. The proposed structure will provide high temperature, high heat flux acquisition and dissipation, as well as providing the structural integrity required to meet mission objectiv ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
  8. Innovative Hydrogen Peroxide Turbopump Design for Affordable Small Launch Vehicles.

    SBC: FRONTIER ASTRONAUTICS, LLC            Topic: Z9

    The concept proposed is that of an innovative turbopump using hydrogen peroxide to drive the turbine. The turbopump has a unique feature in that it has an integral electric generator used to generate electricity and power an external fuel pump.By using hydrogen peroxide decomposed over a catalyst pack only one fluid can be used to drive the turbine. Typically, a turbopump combusts a fuel and an ox ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
  9. HARPOON- High Access Raman Probe with Onboard Optical Numerization

    SBC: Impossible Sensing            Topic: S1

    We propose to build and critically test a TRL4 High Access Raman Probe with Onboard Optical Numerization (HARPOON), a nextgeneration ultra-compact laser Raman Spectrometer equipped with multiplexed fiber optic sensing points.HARPOON#39;s core unit, hosted inside the spacecraft, contains the laser, spectrometer, and electronic modules. The core unit serves two miniature Raman heads, which enable bo ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
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