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Award Data

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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. Continuous Correlations for Complete Boiling Curves of Cryogenic Fluids

    SBC: CREARE LLC            Topic: T14

    Future space exploration missions will rely on in situ production, storage, and transfer of cryogenic rocket propellants. Engineers need accurate and efficient modeling tools to design the next generation of lightweight, efficient cryogenic propellant management devices and processes. Predictive models for key fluid dynamics and heat transfer behavior must be tailored for use with cryogenic propel ...

    STTR Phase II 2023 National Aeronautics and Space Administration
  2. Nonplanar Spaceborne Additively Manufactured Electronics

    SBC: MICRO-PRECISION TECHNOLOGIES, INC.            Topic: T12

    Micro-Precision Technologies, Inc. (MPT), in partnership with the Center for Advanced Microelectronics Manufacturing (CAMM) at Binghamton University, will develop a commercially-ready process for spaceborne additively manufactured electronics (AME) combining the ruggedness and reliability of MPTrsquo;s thick film ceramic technology with the design freedom of CAMMrsquo;s aerosol jet printing techno ...

    STTR Phase I 2023 National Aeronautics and Space Administration
  3. Improved Gradient Modeling at Interfaces for Accurate CFD of Cryogenic Propellant Tanks

    SBC: CREARE LLC            Topic: T14

    Cryogenic propellant production, storage, and transport is critical for future space missions. Engineers need accurate tools to design the next generation of efficient, lightweight components and processes for cryogenic fluid management (CFM). Computational fluid dynamics (CFD) simulations are key for these efforts, but current commercial codes struggle to capture key behavior at liquid-vapor inte ...

    STTR Phase I 2023 National Aeronautics and Space Administration
  4. Localized 3-D Fiber Reinforcement in Carbon and Ceramic Composites

    SBC: North Country Composits LLC            Topic: H5

    This proposal addresses technology for reusable propulsion and vehicle hot structures specified in topic H5.02:Propulsion systems for Commercial Space industry supporting NASA efforts.Upper stage engine systems, such as those for Space Launch System.Lunar/Mars lander descent/ascent propulsion systems.Aerodynamic structures for aeroshells, control surfaces, and leading edges for hypersonic flight v ...

    SBIR Phase II 2023 National Aeronautics and Space Administration
  5. Low Temperature, Low Capacity Cryocooler Technology

    SBC: CREARE LLC            Topic: S16

    Future astrophysics missions require efficient, low temperature cryocoolers to cool advanced instruments or to serve as the upper-stage cooler for sub-Kelvin refrigerators. Potential astrophysics missions include Lynx, Origins Space Telescope, and the Superconducting Gravity Gradiometer. Cooling loads for these missions are 50 to 300nbsp;mW at temperatures of 4 to 10nbsp;K, with additional loads a ...

    SBIR Phase I 2023 National Aeronautics and Space Administration
  6. A Lightweight Freeze-Tolerant Radiator for Extreme Environments

    SBC: CREARE LLC            Topic: Z13

    Future space exploration missions require advanced thermal control systems (TCSs) to dissipate heat from spacecraft, rovers, or habitats to external environments. These thermal control systems must be lightweight, reliable, and able to effectively control cabin and equipment temperatures under widely varying heat loads and ambient temperatures, including the extremes of lunar night. In this contex ...

    SBIR Phase I 2023 National Aeronautics and Space Administration
  7. Low Maintenance Lunar Dust Filtration

    SBC: CREARE LLC            Topic: Z13

    Creare proposes an Autonomous Habitat Filtration System (AHFS) that uses an electrostatic precipitator and autonomous regeneration system to effectively remove dust from habitable environments in long-duration space missions. Currently, HEPA style filters are a bulky consumable that have a large pressure drop across the filter that increases over time from particle loading. Human Lunar and Mars mi ...

    SBIR Phase I 2023 National Aeronautics and Space Administration
  8. Lightweight, Low-Power Cryogenic Valve for Orbital Propellant Management

    SBC: CREARE LLC            Topic: Z10

    Orbital refueling of cryogenic propellants is a key enabling technology that will extend the usable life of spacecraft around Earth and facilitate the next generation of advanced exploration missions. Propellant management on orbit requires advanced propellant tanks, liquid acquisition devices, propellant transfer pumps, space-rated valves, and other subcomponents compatible with common propellant ...

    SBIR Phase I 2023 National Aeronautics and Space Administration
  9. A Compact, Gravity-Insensitive Gas Trap for Extreme Temperature Environments

    SBC: CREARE LLC            Topic: Z2

    NASA is working toward missions involving crewed habitats for extended stays within orbital platforms. Environmental control of these habitats is enabled by use of thermal control systems to maintain conditions within a tight temperature band. These thermal control systems must be highly reliable, lightweight, and able to effectively control cabin and equipment temperatures to within several degre ...

    SBIR Phase II 2023 National Aeronautics and Space Administration
  10. Compressor for Efficient On-Orbit Gas Transfer

    SBC: CREARE LLC            Topic: Z10

    Transfer of gaseous propellant in space is a critical technology for space exploration and for extending the useful life of satellites. A key component needed for in-space refueling is a compressor that can efficiently move gas from a resupply vehicle to the propellant storage vessel on board the receiver vehicle. High efficiency requires a very high pressure ratio, and operation on orbit requires ...

    SBIR Phase II 2023 National Aeronautics and Space Administration
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