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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. A Novel Hydrogen-Fueled Propulsion System

    SBC: Adroit Systems, Inc.            Topic: N/A

    N/A

    SBIR Phase II 1994 National Aeronautics and Space Administration
  2. 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
  3. Laser Brazing Process for Joining Refractory Materials to Dissimilar Metals

    SBC: American Research Corporation of Virginia            Topic: N/A

    N/A

    SBIR Phase II 1994 National Aeronautics and Space Administration
  4. Alchemist- Air Separation Technology Development

    SBC: ANDREWS SPACE, INC.            Topic: N/A

    The Alchemist system we are proposing is a combined-cycle system which reduces Reusable Launch Vehicle (RLV) liftoff weights by a factor of four relative to all-rocket systems. This reduces the weight of major elements (e.g. Jet engines, wing, and landing gear)by 60%, and allows us the margin to use the same principles and advantages commercial airplanes use to achieve very safe operations and low ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  5. Hybrid Structured-Unstructured Grid-Implicit Algorithm for Geometrically Complex Flow Fields

    SBC: Amtec Engineering Inc            Topic: N/A

    N/A

    SBIR Phase II 1994 National Aeronautics and Space Administration
  6. 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 II 2002 National Aeronautics and Space Administration
  7. An Ultrasonic Biocidal System for Hydrophonic Plant Nutrient Solutions

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

    N/A

    SBIR Phase II 1994 National Aeronautics and Space Administration
  8. Solution based 3-D Mesh adaptation for Heat and Mass predictions

    SBC: Cascade Engineering Services, Inc.            Topic: N/A

    In this proposal, a solution-based three-dimensional mesh adaptation procedure is described. The algorithm utilized in our code can very effectively refine the mesh in regions of interest by moving nodes in regions of unchanging flow field for accurate prediction of steady and unsteady pressure and thermal load distributions. Our flow solver interacts with most popular commercial CAD packages thro ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  9. Quantifying Confidence in the Correctness of Parallel or Distributed Software

    SBC: Cigital, Inc.            Topic: N/A

    N/A

    SBIR Phase II 1994 National Aeronautics and Space Administration
  10. Rotational Molding of Thermoplastic Cryogenic Propellant Tanks

    SBC: LUNA INNOVATIONS INCORPORATED            Topic: N/A

    Rotational molding is a low-cost processing scheme used to fabricate large tanks, ducts, and tubes with complicated shapes. Rotational molding of liquid crystal polymer (LCP) resins was successfully demonstrated in the Phase I program, and the proposed Phase II effort will continue development of this process. LCP materials are of interest in application to cryogenic propellant storage because of ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
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