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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY21 is not expected to be complete until September, 2022.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

  1. Wireless Networked Sensors for Remote Monitoring in Propulsion Systems

    SBC: Nanosonic Inc.            Topic: T1301

    This NASA Phase I SBIR program would fabricate wireless networked nanomembrane (NM) based surface pressure sensors for remote monitoring in propulsion systems, using SOI (Silicon on Insulator) NM techniques in combination with our pioneering HybridSil ceramic nanocomposite materials. Such low-modulus, conformal nanomembrane sensor skins with integrated interconnect elements and electronic devices ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  2. Vertical GaN Substrates

    SBC: Sixpoint Materials, Inc.            Topic: DEFOA0000941

    SixPoint Materials will create low-cost, high-quality vertical gallium nitride (GaN) substrates using a multi-phase production approach that employs both hydride vapor phase epitaxy (HVPE) technology and ammonothermal growth techniques to lower costs and maintain crystal quality. Substrates are thin wafers of semiconducting material needed for power devices. In its two-phase project, SixPoint Mate ...

    STTR Phase II 2017 Department of EnergyARPA-E
  3. Unified Representation for Collaborative Visualization and Processing of Terrain Data

    SBC: DigitalFish, Inc.            Topic: T401

    We build upon our prior work applying subdivision surfaces (subdivs) to planetary terrain mapping. Subdivs are an alternative, multi-resolution method with many advantages over conventional digital elevation maps (DEM's) and fixed-resolution meshes. The proposed research is innovative in presenting a new setting for subdivs demanding novel extensions to subdiv algorithms, techniques and theory as ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  4. Unified In-Space Propulsion Framework for Prediction of Plume-Induced Spacecraft Environments

    SBC: CFD Research Corporation            Topic: T102

    Chemical contamination of spacecraft components as well as thermal and force loading from firing liquid propellant thrusters are critical concerns for in-space propulsion applications. Gas molecular contamination and liquid droplet deposition due to incomplete combustion threaten to damage surface materials, sensitive instruments and optical sensors, and poses major risks for mission success. Liqu ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  5. Unified In-Space Propulsion Framework for Prediction of Plume-Induced Spacecraft Environments

    SBC: CFD Research Corporation            Topic: T102

    Chemical contamination of spacecraft components as well as thermal and force loading from firing liquid propellant thrusters are critical concerns for in-space propulsion applications. Gas molecular contamination and liquid droplet deposition due to incomplete combustion threaten to damage surface materials, sensitive instruments and optical sensors, and poses major risks for mission success. Liqu ...

    STTR Phase II 2017 National Aeronautics and Space Administration
  6. Ultra-Compact Transmitter for Space-Based Lidar

    SBC: FIBERTEK, INC.            Topic: T901

    Fibertek, Inc. in partnership with researchers at the Pennsylvania State University Center for Innovative Materials Processing through Direct Digital Deposition (CIMP-3D) are proposing to develop a state of the art, space-qualifiable laser transmitter that meets the requirements of the flash lidar transmitter defined in the 2016 STTR subtopic T9.01, Navigation and Hazard Avoidance Sensor Technolog ...

    STTR Phase I 2016 National Aeronautics and Space Administration
  7. Ultra-Compact Transmitter for Space-Based Lidar

    SBC: FIBERTEK, INC.            Topic: T901

    Fibertek, Inc. in partnership with researchers at the Pennsylvania State University Center for Innovative Materials Processing through Direct Digital Deposition (CIMP-3D) are proposing to develop a state of the art, space-qualifiable laser transmitter that meets the requirements of the flash lidar transmitter defined in the 2016 STTR subtopic T9.01, Navigation and Hazard Avoidance Sensor Technolog ...

    STTR Phase II 2017 National Aeronautics and Space Administration
  8. Tunable Opto-electronic Oscillator Based on Photonic Integration of Ultra-High Q Resonators on a SiN Chip

    SBC: OEWAVES, INC            Topic: T802

    The team comprising OEwaves Inc. and UC Davis offers to develop and demonstrate a SiN-platform integrated photonic circuit suitable for a spectrally pure chip-scale tunable opto-electronic RF oscillator (OEO) that can operate as a flywheel in high precision optical clock modules, as well as radio astronomy, spectroscopy, and local oscillator in radar and communications systems. The effort comprise ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  9. Transient Acoustic Environment Prediction Tool for Launch Vehicles in Motion during Early Lift-Off

    SBC: CFD Research Corporation            Topic: T102

    Launch vehicles experience extreme acoustic loads dominated by rocket exhaust plume interactions with ground structures during lift-off, which can produce damaging vibro-acoustic loads on the vehicle and payloads if not properly understood and mitigated against. Existing capabilities for modeling the turbulent plume physics during early lift-off are too dissipative to accurately resolve the propag ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  10. Torch-Augmented Spark Igniter for Nanosat Launch Vehicle LOX/Propylene Rocket Engine

    SBC: Garvey Spacecraft Corporation            Topic: T101

    The technical innovation proposed here is the introduction of torch-augmented spark ignition for high performance liquid oxygen (LOX) / propylene rocket engines now in development for a future two-stage nanosat launch vehicle. Spark ignition is critical for reliably achieving multiple in-flight restarts of NLV upper stage engines. In addition, this new capability will generate immediate R&D benef ...

    STTR Phase I 2016 National Aeronautics and Space Administration
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