You are here

Award Data

For best search results, use the search terms first and then apply the filters
Reset

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. 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 propulsion devices are highly desirable by NASA and the broader electric propulsion community. Large investments in running the long duration test programs (> 20 kHrs) at NASA GRC can be reduced with computer models and allow more focus on exploring the NEXT ion thruster design for future space missions. The current state of e ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  2. Enhanced Carbon Nanotube Ultracapacitors

    SBC: SCIENTIC INC            Topic: T601

    The proposed innovation utilizes carbon nanotubes (CNTs) coated with pseudo-capacitive MnO2 material as nano-composite electrode and ionic electrolyte for the construction of ultracapacitors. This novel approach of using nano-structured CNTs architectures provides high surface area of attachment of MnO2 nano-particles to maximize the charge efficiency and power capacity and to reduce series resist ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  3. Advanced Simulation Framework for Design and Analysis of Space Propulsion Systems

    SBC: STREAMLINE NUMERICS INC            Topic: T901

    The innovation proposed here is a high-performance, high-fidelity framework in the computational fluid dynamics (CFD) code called Loci-STREAM to enable accurate, fast and robust simulations of unsteady multiphase flows such as combustion involving liquid-gas phases in liquid rocket injectors and solid-gas phases in solid rocket motors, and cryogenic cavitation in delivery systems of liquid rocket ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  4. Multi-Robot Planetary Exploration Architectures

    SBC: AURORA FLIGHT SCIENCES CORPORATION            Topic: T101

    Space policy direction is shifting, particularly with respect to human goals. Given the uncertainty of future missions to the moon, Mars, and other bodies, a tool that allows for informed analysis of the option space is particularly relevant. Aurora Flight Sciences and MIT propose to further develop the Multi-Robot Planetary Exploration Architecture (MRPEA) methodology, a suite of software tools ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  5. Thermal Stir Welding of High Strength and High Temperature Alloys for Aerospace Applications

    SBC: Keystone Synergistic Enterprises, LLC            Topic: T901

    The Keystone and MSU team propose to build on the successful feasibility demonstration conducted during Phase I to complete the development of solid-state joining of high strength and temperature alloys utilizing the Thermal Stir Welding process. The focus alloy for this project is Haynes 230; the alloy of choice typically utilized in rocket engine nozzel skirts. This class of alloy is difficult t ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  6. Ultraefficient Themoelectric Devices

    SBC: MICROXACT INC.            Topic: T801

    Thermoelectric (TE) devices already found a wide range of commercial, military and aerospace applications. However, at present commercially available TE devices typically offer limited heat to electricity conversion efficiencies, well below the fundamental thermodynamic limit, calling for the development of higher efficiency materials. The team of MicroXact Inc., Virginia Tech and Sundew Technolog ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  7. High-Fidelity Gas and Granular Flow Physics Models for Rocket Exhaust Interaction with Lunar Soil

    SBC: CFD RESEARCH CORPORATION            Topic: T701

    Current modeling of Lunar and Martian soil erosion and debris transport caused by rocket plume impingement lacks essential physics from the peculiar granular characteristics of highly irregular regolith particles. Current granular mechanics models are based on mono-disperse spherical particles empiricism unsuitable for capturing the poly-disperse irregularly shaped grain mechanics. CFDRC and the U ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  8. Mission-Aware Payloads for Unmanned Platforms

    SBC: Sentix            Topic: T1502

    Sentix and Brigham Young University propose the research and development of embedded payload intelligence for inflight optimization of surveillance, reconnaissance, and scientific missions. The current proposal leverages a substantial body of scientific and experimental knowledge derived from the Tactical Seeability™ System developed by Sentix' staff and BYU researchers to provide fully automated ...

    STTR Phase I 2013 National Aeronautics and Space Administration
  9. Advanced Deposition Capability for Oxidation&Corrosion Protection Coatings

    SBC: Directed Vapor Technologies International, Inc.            Topic: T1201

    NASA's long range goals of reducing the fuel consumption by 30% and increasing fuel efficiency by 35% can be partially accomplished through increasing engine operation temperatures. As a result, the disk section is desired to operate in increasingly higher temperatures, which will subject it to additional degradation mechanisms of oxidation and hot corrosion. One approach to enhance the tem ...

    STTR Phase I 2013 National Aeronautics and Space Administration
  10. OrFPGA: An Empirical Performance Tuning Tool for FPGA Designs

    SBC: RNET TECHNOLOGIES INC            Topic: T1101

    With the capacity and performance of FPGAs suitable for space borne applications continuously increasing, the design of FPGAs is becoming increasingly complex involving trading off or simultaneous optimization of space, speed, and power. RNET and ANL are proposing to develop software infrastructure that facilitates automatic performance tuning of FPGAs in terms of speed, power, and size. We introd ...

    STTR Phase I 2013 National Aeronautics and Space Administration
US Flag An Official Website of the United States Government