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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

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. Antistatic Thermal Control Coatings

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Electrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  2. Antistatic Thermal Control Coatings

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Electrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  3. Self-Deploying Foam Antenna Structures

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Inflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...

    STTR Phase I 2002 National Aeronautics and Space Administration
  4. Self-Deploying Foam Antenna Structures

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Inflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...

    STTR Phase II 2002 National Aeronautics and Space Administration
  5. Spacesuit Monitor

    SBC: Adherent Technologies, Inc.            Topic: N/A

    The concentration of carbon dioxide in exhaled breath is 3.8%; a concentration of 2% causes deepened breathing, and 4% causes a marked increase in respiration. These higher concentrations of CO2 also cause drowsiness and can be unsafe. Therefore, it is desirable to monitor the concentration of CO2 in exhaled breath to guarantee the safety of an astronaut in the dangerous extravehicular environment ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  6. Energy Efficient Cryogenic Transfer Line with Magnetic Suspension

    SBC: Amac International, Inc.            Topic: N/A

    Energy efficient, cost effective, cryogenic distribution system (up to several miles) is strongly commanded for spaceport and in-space cryogenic systems. The use of magnetic levitation by permanent magnets and high temperature superconductors (HTS) results in without mechanical contact and thus, the conduction part of the heat leak can be reduced to zero. In Phase I, various magnetic suspensions, ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  7. Energy Efficient Cryogenic Transfer Line with Magnetic Suspension

    SBC: Amac International, Inc.            Topic: N/A

    Energy efficient, cost effective, cryogenic distribution system (up to several miles) is strongly commanded for spaceport and in-space cryogenic systems. The use of magnetic levitation by permanent magnets and high temperature superconductors (HTS) results in without mechanical contact and thus, the conduction part of the heat leak can be reduced to zero. In Phase I, various magnetic suspensions, ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  8. Magnetohydrodynamic Stable Reference (MSTAR)

    SBC: A-TECH CORPORATION            Topic: N/A

    Platforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  9. Magnetohydrodynamic Stable Reference (MSTAR)

    SBC: A-TECH CORPORATION            Topic: N/A

    Platforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  10. Reconfigurable Guidance for Reusable Launch Vehicles

    SBC: BARRON ASSOCIATES, INC.            Topic: N/A

    The flight envelope for X-34 ranges from subsonic to hypersonic with altitudes up to 50 miles. Designing a guidance law that performs across this broad flight envelope presents several challenges. Robustness to uncertain aerodynamics is of paramount importance because of the sparse amount of wind tunnel and flight test data that exists for reusable launch vehicles at hypersonic Mach numbers. The n ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
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