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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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.

The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.

  1. Near-Real-Time Integration of Soil State Information

    SBC: CREARE LLC            Topic: A17130

    The Army requires the development of models for improving the state-of-the-art understanding of soil state characteristics in regions with varying observational input datasets. Currently, weather-scale remote sensing, mesoscale standoff sensing, and point-scale in situ sensing provide approximate measurements of near-surface soil moisture at different scales and extents of coverage. In addition, s ...

    SBIR Phase I 2018 Department of DefenseArmy
  2. Metamorphic Buffer Layer Growth for Bulk InAs(x)Sb(1-x) LWIR Detectors

    SBC: QMAGIQ LLC            Topic: A16AT009

    Bulk InAs(x)Sb(1-x) is an infrared detector material that promises higher quantum efficiency than antimony-based superlattices in the longwave infrared (LWIR). This is due to the longer diffusion length of minority carrier holes in the bulk than in superlattices where they are localized. No native substrate exists for lattice-matched growth of InAs(x)Sb(1-x) material with LWIR bandgaps. So a key c ...

    STTR Phase II 2018 Department of DefenseArmy
  3. Multi-Spectral Infrared Focal Plane Array For Wildfire And Burning-Biomass Analysis

    SBC: QMAGIQ LLC            Topic: S1

    An important NASA mission is to remotely analyze fires, such as wildfires and burning biomasses, for their chemical content. The chemical species of most interest have infrared spectral signatures at wavelengths ranging from 1.5 microns to 12 microns. A broadband infrared focal plane array (FPA) with that spectral coverage and high quantum efficiency is a key technology to enable this mission. Qma ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  4. Optically Interrogated Thin Film Strain Gauge for Balloon

    SBC: CREARE LLC            Topic: S3

    To support development of atmospheric balloons and gossamer structures, NASA requires a capability for real-time, dynamic strain measurement in thin polymeric membranes during deployment and flight. This capability will provide quantitative test data to inform balloon design efforts, as well as enable real-time monitoring of material state during flight. Existing technologies include wired or wi ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  5. High Efficiency 4 K Cryocooler for Space Missions

    SBC: CREARE LLC            Topic: S1

    Future astrophysics missions require efficient, low-temperature cryocoolers to cool advanced instruments or serve as the upper stage cooler for sub-Kelvin refrigerators. Potential astrophysics missions include Lynx, the Origin Space Telescope, and the Superconducting Gravity Gradiometer. Cooling loads for these missions are up to 300 mW at temperatures of 4 to 10 K, with additional loads at higher ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  6. ASOMIS

    SBC: APPLIED GEOSOLUTIONS LLC            Topic: S5

    The innovation of the Agricultural SOil Moisture and Irrigation Status (A·SOM·IS) platform is the development of operational and moderate resolution mapping and assessment of soil moisture, irrigation status (irrigated vs not), and crop water stress metrics at field scale for agricultural decision support tools. The platform focuses on utilization of Synthetic Aperture Radar (SAR) and blends SAR ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  7. A Compact, Lightweight Electrically Driven Propellant Pump with High Pressure Rise

    SBC: CREARE LLC            Topic: S4

    Reducing the inert mass of propulsion systems in sample return spacecraft will reduce their launch costs and increase opportunity for these missions. Compared to a pressure-fed system, a propellant pump-fed system can significantly reduce overall propulsion system mass, especially for a system with high propellant throughput. To address this need, we propose to develop a compact, lightweight elect ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  8. Integrated Silicon Carbide Electronics for Venus Surface Actuation

    SBC: OZARK INTEGRATED CIRCUITS INC            Topic: S4

    NASA has demonstrated a resolve for a flagship mission in the coming years to revisit Venus and land instruments on the surface. Venus has a corrosive, high-pressure (~100 bar), high-temperature (470°C) environment. A motor drive is the major theme that runs through the most critical needs for optimum geological and atmospheric exploration on Venus.An electronically-controlled motor, operating at ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  9. A 128-Channel Compact VUV Spectrometer for Wide-Temperature Entry Descent & Landing Sensing Applications

    SBC: OZARK INTEGRATED CIRCUITS INC            Topic: Z7

    NASA manned and robotic missions to the surface of planetary or airless bodies require Entry, Descent, and Landing (EDL). For many of these missions, EDL represents one of the riskiest phases of the mission. Despite the criticality of the EDL phase, NASA has historically gathered limited engineering data from such missions, and use of the data for real-time Guidance, Navigation and Control (GN&C) ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  10. Lightweight, Reliable Cryogenic Screen Channel Acquisition Devices with High Expulsion Efficiency

    SBC: CREARE LLC            Topic: Z10

    Refueling spacecraft in space offers tremendous benefits for increased spacecraft payload capacity and reduced launch cost. However, in a microgravity environment, acquiring vapor-free cryogenic liquid propellants from supply tanks and then transferring them to receiving tanks of a rocket engine is very challenging. To address this challenge, we propose to develop a robust, lightweight cryogenic s ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
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