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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. Power Generating Coverings and Casings

    SBC: STREAMLINE AUTOMATION LLC            Topic: T301

    Advances in structured heterogeneity together with nanomaterials tailoring has made it possible to create thermoelectrics using high temperature, polymer composites. While such thermoelectrics do not have the capability to approach the efficiency of top performing ceramic modules such as BiTe, they do provide two unique aspects of use in energy scavenging: the ability to conform to irregular large ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  2. High Performance Hybrid Upper Stage for NanoLaunch Vehicles

    SBC: PARABILIS SPACE TECHNOLOGIES INC            Topic: T101

    Parabilis Space Technologies, Inc (Parabilis), in collaboration with Utah State University (USU), proposes further development of a low-cost, high-performance launch vehicle upper stage that uses a high density, storable oxidizer and a polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This effort will build upon the successful opti ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  3. The World is Not Enough (WINE): Harvesting Local Resources for Eternal Exploration of Space

    SBC: Honeybee Robotics, Ltd.            Topic: T402

    The World is Not Enough (WINE) is a new generation of CubeSats that take advantage of ISRU to explore space. The WINE takes advantage of existing CubeSat technology and combines it with 3D printing technology and an In Situ Resource utilization (ISRU) water extraction system. 3D printing enables development of steam thrusters (higher Isp than cold gas) as well as tanks that fit within the availabl ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  4. Integrated Monitoring AWAReness Environment (IM-AWARE)

    SBC: AMERICAN GNC CORPORATION            Topic: T1301

    American GNC Corporation (AGNC) and Louisiana Tech University (LaTECH) are proposing a significant breakthrough technology, the Integrated Monitoring AWAReness Environment (IM-AWARE) consisting of an Enterprise Infrastructure with closely coupled smart sensor networks and Enhanced IT Security to enable: (i) real time monitoring of the distribution systems health; (ii) supporting maintenance operat ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  5. A Coupled System for Predicting SPE Fluxes

    SBC: PREDICTIVE SCIENCE INCORPORATED            Topic: T602

    Solar Particle Events (SPEs) represent a major hazard for extravehicular maneuvers by astronauts in Earth orbit, and for eventual manned interplanetary space travel. They can also harm aircraft avionics, communication and navigation. We propose to develop a system to aid forecasters in the prediction of such events, and in the identification/lengthening of "all clear" time periods when there is ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  6. Advanced Gas Sensing Technology for Space Suits

    SBC: INTELLIGENT OPTICAL SYSTEMS, INC.            Topic: T601

    The gas sensor in the PLSS of the ISS EMU will meet its projected life in 2020, and NASA is planning to replace it. At present, only high TRL devices based on infrared absorption are candidate replacements, because of their proven long-term stability, despite their size and power consumption and failures in the presence of liquid water. No current compact sensor has the tolerance for liquid water ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  7. Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM)

    SBC: CHROMOLOGIC LLC            Topic: T801

    Chromologic (CL) and the California Institute of Technology (Caltech) propose to continue the Phase II STTR development and demonstration of a Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM) instrument that transmits high energy beams of electrons sequentially using a two-dimensional array of multiple, miniaturized electron probes into a planetary atmosphere and strike ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  8. Improved Forecasting of Solar Particle Events and their Effects on Space Electronics

    SBC: CFD RESEARCH CORPORATION            Topic: T602

    High-energy space radiation from Galactic Cosmic Rays and Solar Particle Events (SPEs) pose significant risks to equipment and astronaut health in NASA missions. Energetic particles from SPEs associated with flares and coronal mass ejections (CMEs) may adversely affect not only beyond-Low-Earth-Orbit missions, but also aircraft avionics, communications, and airline crew/passenger health. It is cru ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  9. Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design

    SBC: M4 ENGINEERING, INC.            Topic: T401

    We propose the development of a novel aerodynamic modeling approach making use of fully unstructured grids for unsteady panel aerodynamic models for aeroelastic and aeroservoelastic analysis. The unsteady aerodynamic code will be integrated with an existing suite of aeroelastic and aeroservoelastic analysis tools making it possible to perform aeroelastic and aeroservoelastic analysis of complex v ...

    STTR Phase II 2016 National Aeronautics and Space Administration
  10. Particle Flow Physics Modeling for Extreme Environments

    SBC: CFD RESEARCH CORPORATION            Topic: T403

    The liberation of particles induced by rocket plume flow from spacecraft landing on unprepared regolith of the Moon, Mars, and other destinations poses high mission risks for robotic and human exploration activities. This process occurs in a combination of "extreme environments" that combine low gravity, little or no atmosphere, rocket exhaust gas flow that is supersonic and partially rarefied, an ...

    STTR Phase II 2014 National Aeronautics and Space Administration
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