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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. 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
  4. 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
  5. 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
  6. 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
  7. Solid-fueled Micro Colloid Thruster

    SBC: TDA RESEARCH, INC.            Topic: T301

    Nanosatellites are receiving increased interest since they are proving reliable for surveillance, communication and other space missions. Also, the possibility of launching "constellations" of them offers unique capabilities for low-cost experimentation, sensing and communications in space. In comparison to larger spacecraft, their development time and costs have reduced and their launch costs a ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  8. A Self-Regulating Freezable Heat Exchanger for Spacecraft

    SBC: TDA RESEARCH, INC.            Topic: T601

    A spacecraft thermal control system must keep the cabin (both air and its structure if manned) and electronic equipment within a narrow temperature range even though the environment may vary from very cold to warmer than room temperature. Since water is safe to use and an excellent coolant (other than its high freeze point and volumetric expansion during freeze), a water coolant loop often is use ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  9. Intelligent Radiative Materials

    SBC: PC KRAUSE & ASSOCIATES INC            Topic: T1002

    An opportunity to boost energy efficiency in homes and buildings exists through the design of functional radiative properties in glass and other building materials. Current surface materials ignore or take first-order approaches to complicated spectral behavior, leading to sub-optimal properties. The sensitivity of material properties to microscale surface structuring creates a design challenge ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  10. Improved Forecasts of Solar Particle Events using Eruptive Event Generators based on Gibson-Low and Titov-Demoulin Magnetic Configurations

    SBC: MICHIGAN AEROSPACE CORP            Topic: T602

    Radiation hazards constitute a serious risk to human and robotic space operations beyond Low-Earth orbit. Primary contributors to space radiation include Solar Particle Events (SPEs) associated with Coronal Mass Ejections (CMEs). Because the mechanisms that produce coronal mass ejections (CME) are exceedingly complex, no reliable deterministic methods for predicting eruptions are yet available, a ...

    STTR Phase I 2015 National Aeronautics and Space Administration
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