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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. Anion Exchange Resin for Chirality-based Separation of Single-wall Carbon Nanotubes

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

    Sepax Technologies, Inc. has identified a new type of anoin-exchange resin which separates single-wall carbon nanotubes (SWCNTs) with >80% recovery yield and resolves in a single pass the chiral tubes of (6,5) well from commercial SWCNT starting materials by Chromatography. Improvement and scale up of the targeted resin production will facilitate the separation of chiral nanotubes for the academic ...

    SBIR Phase II 2012 Department of CommerceNational Institute of Standards and Technology
  2. An Electrochemical, Point-of-Care Detector for Reagent-free, In-situ Diagnostics of Pathogens

    SBC: CFD RESEARCH CORPORATION            Topic: T102

    For long-term exploratory space travel, there will be a critical need for in-situ diagnosis and assessment of biological specimens from symptomatic astronauts, especially, disease pathogens (virus, bacterium, or fungus) and microbial contaminants. Hence, a real-time, non-culture-based microbial detection, identification and quantification system for on-flight monitoring and evaluation of pathogens ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  3. Autonomous Multi-Robot Exploration using UWB

    SBC: TDC Acquisition Holdings, Inc.            Topic: T801

    Single multi-sensor teleoperated systems are not optimal for NASA exploratory missions because they limit the coverage area and scope of exploration and create a single point for mission failure. A better solution would use many robots cooperating to maximize exploration area and location accuracy while minimizing total system power and weight. The goal of this research is to investigate pulsed ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  4. A Multi-disciplinary Tool for Space Launch Systems Propulsion Analysis

    SBC: CFD RESEARCH CORPORATION            Topic: T901

    An accurate predictive capability of coupled fluid-structure interaction in propulsion system is crucial in the development of NASA's new Space Launch System (SLS). This STTR effort will develop a multi-disciplinary tool to improve CFD prediction capability in modeling coupled fluid structure interaction (FSI) phenomena for many SLS propulsion applications such as flexible inhibitors for SRMs ...

    STTR Phase I 2012 National Aeronautics and Space Administration
  5. Ionomer-membrane Water Processor System Design and EDU Demonstration

    SBC: PARAGON SPACE DEVELOPMENT CORPORATION            Topic: X301

    a. Paragon Space Development Corporation¿ (Paragon) proposes to continue our investigation into the use of microporous-ionomer membrane technology to improve the robustness and effectiveness and simplify water recovery processes for space applications. Improved robustness and effectiveness will be evident through (1) reduced loading onthe downstream post processor due to the ionomer¿s unique pr ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  6. Improved Rhenium Thrust Chambers for In-Space Propulsion

    SBC: Plasma Processes, LLC            Topic: S304

    Radiation-cooled, bipropellant thrust chambers are being considered for the ascent/descent engines and reaction control systems for NASA missions such as Mars Sample Return and Orion MPCV. Currently, iridium-lined rhenium combustion chambers are the state-of-the-art for in-space engines. NASA's Advanced Materials Bipropellant Rocket (AMBR) engine, a 150-lbf iridium-rhenium chamber produced by Pla ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  7. Non-Toxic HAN Monopropellant Propulsion

    SBC: Plasma Processes, LLC            Topic: X202

    Non-toxic monopropellants have been developed that provide better performance than toxic hydrazine. Formulations based on hydroxylammonium nitrate (HAN) have superior performance as compared to hydrazine with Isp (261 seconds, 12% greater), higher density and volumetric impulse (60% greater density-impulse), lower melting point, and much lower toxicity (No self contained breathing apparatus requir ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  8. Frequency-Locked Single-Frequency Fiber Laser at 2 Micron

    SBC: ADVALUE PHOTONICS INC            Topic: S101

    Frequency-locked single-frequency 2 micron fiber laser is proposed to be used for airborne/spaceborne coherent lidar measurements, i.e., Active Sensing of CO2 Emissions over Nights, Days, and Seasons. The laser is based on our proprietary fiber technology and extensive experience in fiber laser development, which features a compact, highly stable, frequency-stabilized light source. Advanced freque ...

    SBIR Phase II 2012 National Aeronautics and Space Administration
  9. Emile: The EventML Explorer

    SBC: ATC-NY INC            Topic: A120

    The protocols needed to coordinate the activities of distributed components, such as consensus algorithms, are notoriously difficult to design, implement, and verify. Abstraction is the only way to gain intellectual control over this complex problem; so ATC-NY and Cornell University have developed Event Logic, a high-level model for describing and reasoning about distributed systems, and EventML, ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  10. Predictive Gust Load Alleviation Control Using Leading Edge Stagnation Point Sensor

    SBC: ZONA TECHNOLOGY INC            Topic: A207

    ZONA Technology, Inc. proposes an R & D effort to develop a Gust Load Alleviation (GLA) control system using a novel Leading Edge Stagnation Point (LESP) sensor that has the nearly instantaneous predictive capability. The real-time gust information from the sensor will enhance the performance of the proposed GLA control system. The GLA control method we will adopt is the Generalized Predictive Con ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
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