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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. Intelligent Control For Autonomous Remote Spacecraft

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    We will apply the latest knowledge in learning control, adaptive control, and optimal control to develop a modular, state-of-the-art, adaptive, nonlinear, guidance, navigation, and control package for remote spacecraft. The system will incorporate planning and decision making modules to give the remote spacecraft on-line goal directed self-reliant behavior with a high degree of autonomy. At the hi ...

    STTR Phase I 2001 National Aeronautics and Space Administration
  2. MagLev Launch Propulsion for LoFLYTE¿Waverider Unmanned Aerial Vehicle

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation, teamed with PRT Advanced Maglev Systems, will work together to perform flight test experiments for launching the LoFLYTE¿ UAV from NASA Marshall Space Flight Center¿s 100-foot outdoor Maglev track. The goal of the Phase I program is to lay the foundation for a Phase II flight test program that will demonstrate the use of the Maglev track to launch a hypersonic configuration ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  3. Friction Drag Reduction System

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation Corporation proposes to design a system for reducing the friction drag on an aircraft by introducing an ion space charge into the aircraft¿s boundary layer. We will develop a detailed model for the drag reduction mechanism; evaluate the system performance; evaluate alternative electromagnetic and/ or mechanical processes for generating a space charge in the boundary layer of a ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  4. Friction Drag Reduction System

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation Corporation proposes to design a system for reducing the friction drag on an aircraft by introducing an ion space charge into the aircraft¿s boundary layer. We will develop a detailed model for the drag reduction mechanism; evaluate the system performance; evaluate alternative electromagnetic and/ or mechanical processes for generating a space charge in the boundary layer of a ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  5. Superconducting Magnetic Energy Storage for Maglifter Launch Assist

    SBC: Advanced Magnet Lab, Inc.            Topic: N/A

    NASA is considering an electromagnetic catapult, the MagLifter to lowerthe cost of cargo delivery to space and improve launch reliability. Acarrier sled, levitated and propelled by magnets, provides an inintialvelocity to a space transportation vehicle. For Large payloads, therequired energy for this launch assist is in the range of 20 gigajoulewith peak-power requirements of several gigawatt.Usin ...

    STTR Phase I 2001 National Aeronautics and Space Administration
  6. Universal Superconducting Magnets for MagLifter Launch Assist Sleds

    SBC: Advanced Magnet Lab, Inc.            Topic: N/A

    NASA is considering an electromagnetic catapult, the MagLifter to lowerthe cost of cargo delivery to space. A carrier sled levitated and propelledby magnets provides the initial velocity to a space transportation vehicle.Superconducting magnets enable higher fields at lower weights than normalconducting magnets and consequently a significantly larger clearancebetween the guideway and the carrier s ...

    STTR Phase I 2001 National Aeronautics and Space Administration
  7. Universal Superconducting Magnets for MagLifter Launch Assist Sleds

    SBC: Advanced Magnet Lab, Inc.            Topic: N/A

    NASA is considering an electromagnetic catapult, the MagLifter to lowerthe cost of cargo delivery to space. A carrier sled levitated and propelledby magnets provides the initial velocity to a space transportation vehicle.Superconducting magnets enable higher fields at lower weights than normalconducting magnets and consequently a significantly larger clearancebetween the guideway and the carrier s ...

    STTR Phase II 2001 National Aeronautics and Space Administration
  8. Biomimetics Based Design of Damage Tolerant Airframe Panels

    SBC: AeroChem Corporation            Topic: N/A

    The specific innovation proposed is to design an advanced composite airframe panel for damage tolerance by incorporating biologic solutions to a similar problem found in nature, using a biomimetic approach. We will identify principal material (fiber) directions and density profiles about naturally occurring holes in bones through a microscopic and radiographic techniques. These holes are known to ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  9. Biomimetics Based Design of Damage Tolerant Airframe Panels

    SBC: AeroChem Corporation            Topic: N/A

    The specific innovation proposed is to design an advanced composite airframe panel for damage tolerance by incorporating biologic solutions to a similar problem found in nature, using a biomimetic approach. We will identify principal material (fiber) directions and density profiles about naturally occurring holes in bones through a microscopic and radiographic techniques. These holes are known to ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  10. Low Cost Engine Test Stand for 500 lb Thrust Class Engines

    SBC: AJT and Associates, Inc            Topic: N/A

    AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard test-stand interface, greatly reducing the time required to install and remove various engines. Thi ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
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