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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. Advanced Particle-in-Cell (PIC) Tools for Simulation of Electrodynamic Tether Plasma Interactions

    SBC: TECH-X CORPORATION            Topic: T301

    Electrodynamic tethers are optimally suited for use in Low-Earth-Orbit (LEO) to generate thrust or drag maneuver satellites. LEO region is polluted with space debris from the left over of rockets and abandoned satellites. It becomes important to clean them, i.e., de-orbit and ED tethers are promising for such applications. ED tethers are operating without propellants, so less polluting in our spac ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  2. Non-Catalytic Self Healing Composite Material Solution

    SBC: ADA TECHNOLOGIES, INC.            Topic: T901

    Fiber reinforce polymer (FRP) composite materials are seeing increasing use in the construction of a wide variety of aerospace structures. However, uncertainties regarding the material's impact durability continue to plague the FRP composites community. To address this need, ADA Technologies, Inc. (ADA), Littleton, CO, in partnership with the University of Delaware's Center for Composi ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  3. Advanced Flow Analysis Tools for Transient Solid Rocket Motor Simulations

    SBC: Tetra Research Corporation            Topic: T901

    The challenges of designing, developing, and fielding man-rated propulsion systems continue to increase as NASA's mission moves forward with evolving solid propulsion requirements. Recent developments in simulating solid rocket motor environments include Lagrangian particle tracking, particle combustion models, dynamic particle drag and breakup models, and two phase impingement phenomena. T ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  4. Helium-Hydrogen Recovery System

    SBC: TDA RESEARCH, INC.            Topic: T1002

    Immense quantities of expensive liquefied helium are required at Stennis and Kennedy Space Centers for pre-cooling rocket engine propellant systems prior to filling with liquid hydrogen, for pressurizing tanks and for safely purging residual hydrogen. Presently, the helium used in these processes is discarded, along with substantial quantities of hydrogen. TDA Research proposes to design and build ...

    STTR Phase I 2011 National Aeronautics and Space Administration
  5. High Power High Thrust Ion Thruster (HPHTion): 50 CM Ion Thruster for Near-Earth Applications

    SBC: Electrodynamic Applications Inc            Topic: T301

    Advances in high power, photovoltaic technology has enabled the possibility of reasonably sized, high specific power, high power, solar arrays. At high specific powers, power levels ranging from 50 to several hundred kW are feasible. Coupled with gridded ion thruster technology, this power technology can be mission enabling for a wide range of missions ranging from ambitious near Earth NASA miss ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  6. Next-Generation Ion Thruster Design Tool to Support Future Space Missions

    SBC: TECH-X CORPORATION            Topic: T301

    Computational tools that accurately predict the performance of electric propulsiondevices are highly desirable and beneficial to NASA and the broader electric propulsioncommunity. The current state-of-the-art in electric propulsion modeling relies heavily onempirical data and on numerous computational "knobs". In Phase I of this project, wedeveloped the most detailed ion engine discharge chamber m ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  7. Efficient Quantification of Uncertainties in Complex Computer Code Results

    SBC: ILLINOISROCSTAR LLC            Topic: T501

    Propagation of parameter uncertainties through large computer models can be very resource intensive. Frameworks and tools for uncertainty quantification are generally geared to individual codes, are research codes, or are single-purpose tools such as LHS matrix generators. The Reduced-Order-Clustering-Uncertainty-Quantification (ROCUQ) methodology discussed in this proposal is specifically designe ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  8. One-Sided 3D Imaging of Non-Uniformities in Non-Metallic Space Flight Materials

    SBC: TeraMetrix, LLC            Topic: T701

    In this Phase II project, we propose to develop, construct, and deliver to NASA a prototype single-sided computed tomography time-domain terahertz (single-sided CT TD-THz) scanner accessory. This accessory will be suitable to be mounted onto a non-destructive evaluation (NDE) imaging gantry for the single-sided inspection of spacecraft and launch vehicle composite structures. The single-sided CT ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  9. An Automated High Aspect Ratio Mesher for Computational Fluid Dynamics

    SBC: Ciespace Corporation            Topic: T801

    The work will focus on the 3D implementation of the Phase 1 CHARM mesher, with solution-adaptive iteration for CFD and non-CFD applications. The proposed 3D method will incorporate and extend a previously developed method of generating field-guided hexahedral elements from a metric tensor field. While the fundamental technical approach?a combination of metric tensor conditioning, metric-tracing me ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  10. High Efficiency Flexible Photovoltaic Blankets

    SBC: MICROLINK DEVICES INC            Topic: AF10BT05

    ABSTRACT: MicroLink proposes a device that combines ultra-thin, high-efficiency, GaAs-based multijunction solar cells, made using our proprietary epitaxial lift-off (ELO) process, with a novel packaging approach that will result in high-efficiency, flexible photovoltaic blankets. MicroLink has developed a process that produces ultra-thin, flexible solar cells. In this project, these flexible so ...

    STTR Phase I 2011 Department of DefenseAir Force
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