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Award Data

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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 Hybrid Stage

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T101

    The proposed technology builds off GTL's advanced solid ramjet fuel. The method uses additive manufacturing methods to produce an innovative new type of fuel grain that regresses quickly and has a high Isp and combustion efficiency. With this technology, the performance of a liquid rocket engine can be had with a hybrid rocket system. This technology allows for a simple, low cost, high performanc ...

    STTR Phase I 2015 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 a low cost, high performance launch vehicle upper stage using oxygen and a novel additively manufactured polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This technology will fulfill the ever-growing mission demands of the C ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  3. Multi Domain Modeling for Space Systems

    SBC: METAMORPH INC            Topic: T1102

    A comprehensive model-based approach will be enabled for space systems design via the work started on Phase I of this project. The OpenMETA toolkit is a cyber-physical modeling tool for the design and virtual integration of complex systems, developed under the DARPA AVM Program. OpenMETA will be leveraged and extended to support NASA/JPL goals for multi-physics, multi-domain modeling, analysis, ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  4. Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM)

    SBC: CHROMOLOGIC LLC            Topic: T801

    Chromologic (CL) and the California Institute of Technology (Caltech) propose to develop and demonstrate a Multifunctional Environmental Digital Scanning Electron Microprobe (MEDSEM) instrument that transmits high-energy beams of electrons sequentially from a two-dimensional array of miniaturized electron probes into a planetary atmosphere, and these electrons will strike solid or liquid planetary ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  5. Multi-Disciplinary Analysis and Optimization of Integrated Spacecraft System Models

    SBC: M4 ENGINEERING, INC.            Topic: T1102

    M4 Engineering and Missouri S&T propose to investigate the viability of creating a multidisciplinary analysis and optimization architecture for analyzing spacecraft system models. The current approach will utilize commercial off-the-shelf (COTS) software to alleviate acquisition hurdles for NASA (and public) technical monitors/reviewers. Next, a preliminary set of analysis modules will be develo ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  6. Integrated Monitoring AWAReness Environment (IM-AWARE)

    SBC: AMERICAN GNC CORPORATION            Topic: T1301

    For this STTR project, American GNC Corporation (AGNC) and Louisiana Tech University (LaTECH) are proposing a significant breakthrough technology for improving embedded sensing, remote and wireless monitoring, and the capture of data, information, and knowledge (DIaK) at propulsion ground test facilities with the Integrated Monitoring AWAReness Environment (IM-AWARE). This system consists of smart ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  7. Ultra Large Core High Energy Fiber Amplifier

    SBC: POLARONYX INC            Topic: T901

    Laser transmitters operating at a pulse repetition rate of 20 Hz to 50 Hz and with pulse energy from 30 - 50 mJ have been considered to be an enabling technology for CO2 measurement and optical communications. PolarOnyx proposes a novel approach targeting to make reliable high energy ultra large core fiber amplifier at 1.57 micron and employing our proprietary technologies in specialty fibers, spe ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  8. Fiber Optic Acoustic Emission System for Structural Health Monitoring of Composite Pressure Vessels

    SBC: VERAPHOTONICS INC            Topic: T1201

    Pressurized systems and pressure vessels used in NASA ground-based and flight-based applications including fuel tanks, composite overwrapped pressure vessels (COPVs), and composite tankage commonly suffer from several types of degradation including fatigue, cracking, lack of bonding, and leakage. Veraphotonics proposes to develop a pressure vessel leak and damage detection system. In a large vesse ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  9. An End-To-End Microfluidic Platform for Engineering Life Supporting Microbes in Space Exploration Missions

    SBC: HJ SCIENCE & TECHNOLOGY INC            Topic: T601

    HJ Science & Technology (HJS&T) and Lawrence Berkeley National Laboratory (LBNL) propose a highly integrated, programmable, and miniaturized microfluidic automation platform capable of running rapid and complex synthetic biology and bioengineering processes for engineering life supporting microbes in space exploration missions. Our approach combines the microfluidic automation technology of HJS&T ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  10. Dynamic ASE Modeling and Optimization of Aircraft with SpaRibs

    SBC: M4 ENGINEERING, INC.            Topic: T401

    In aircraft design, reducing structural weight is often a prime objective, while various constraints in multiple disciplines, such as structure, aerodynamics and aeroelasticity should be imposed on the aircraft. Therefore, engineers need optimization tools to incorporate the multidisciplinary constraints using appropriate fidelity during the early stages of concept design. Classic structural desi ...

    STTR Phase II 2015 National Aeronautics and Space Administration
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