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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY22 is not expected to be complete until September, 2023.

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.

  1. 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
  2. High-Fidelity Prediction of Launch Vehicle Lift-off Acoustic Environment

    SBC: CFD RESEARCH CORP            Topic: T101

    Launch vehicles experience extreme acoustic loads during liftoff driven by the interaction of rocket plumes and plume-generated acoustic waves with ground structures. Currently employed predictive capabilities are too dissipative to accurately resolve the propagation of waves throughout the launch environment. Higher fidelity non-dissipative analysis tools are critically needed to design mitigatio ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  3. 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
  4. Improved Models for Prediction of Locally Intense Aeroacoustic Loads and Vibration Environments

    SBC: ATA Engineering, Inc.            Topic: T1201

    ATA Engineering, Inc. proposes an STTR program to develop innovative tools and methods that will significantly improve the accuracy of random vibration response predictions for aerospace structures under critical inhomogeneous aeroacoustic loads. This will allow more accurate predictions of structural responses to be made, potentially reducing vehicle weight and cost and improving the reliability ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  5. ACE Booster

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: T102

    GTL has been developing a suite of transformational technologies that have the capability to disrupt the traditional launch vehicle paradigm. BHL composite cryotank technology provides a four times improvement over large aluminum iso-grid tanks, offering a 6 percentage point improvement in small stage PMF. Superior Stability Engine is an innovative liquid rocket engine configured to maximize comb ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  6. Multiple High-Fidelity Modeling Tools for Metal Additive Manufacturing Process Development

    SBC: CFD RESEARCH CORP            Topic: T1204

    Despite the rapid commercialization of additive manufacturing technology such as selective laser melting, SLM, there are gaps in process modeling and material property prediction that contribute to slow and costly process development, process qualification and product certification. To address these gaps, CFDRC and our partner Dr. Kevin Chou, University of Alabama, will develop multiple computatio ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  7. MEMS Based Solutions for an Integrated and Miniaturized Multi-Spectrum Energy Harvesting and Conservation System

    SBC: Radiance Technologies, Inc.            Topic: T301

    The objective of this proposal is to integrate three unique energy harvesting technologies utilizing our existing research strengths that will be of interest and utility to NASA applications and environmental conditions. By developing multiple technologies, NASA will be able to harvest energy from multiple waste energy sources, namely environmental vibrations, thermal energy, and solar flux. These ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  8. An LED-Based, Laboratory-Scale Solar Simulator for Advanced 3, 4, 5 & 6 Junction Space Photovoltaic Power Systems

    SBC: Angstrom Designs, Inc.            Topic: T201

    As a result of significant technical effort, the Phase I was successful in delivering a solar simulator prototype that not only proved the initial concept but will significantly reduce future risk and increase our ability to deliver a fully-functional solar simulator in Phase II. The proposed innovation is an LED-based, laboratory-scale, solar simulator. The proposed innovation simulates AM0 re ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  9. Modular Electric Propulsion Test Bed Aircraft

    SBC: ROLLING HILLS RESEARCH CORP            Topic: T901

    A hybrid electric aircraft simulation system and test bed is proposed to provide a dedicated development environment for the rigorous study and advancement of hybrid electric powered aircraft. The new test bed and simulation system will provide a dedicated platform and set of analysis tools to study, design, and test hybrid electric powered propulsion components and systems for use in commercial, ...

    STTR Phase II 2014 National Aeronautics and Space Administration
  10. Attitude Control Enhancement Using Distributed Wing Load Sensing for Dynamic Servoelastic Control

    SBC: Systems Technology, Inc.            Topic: T402

    Strain sensor information is used in nature to achieve robust flight, good rejection of wind disturbances, and stable head motion. Similar man-made sensing devices will be used to demonstrate flight control using Fly-by-Feel, with the overall objective of achieving similarly good performance with piloted and autonomous vehicles. The Phase I work demonstrated the feasibility of using strain sensor ...

    STTR Phase II 2014 National Aeronautics and Space Administration
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