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The Award database is continually updated throughout the year. As a result, data for FY21 is not expected to be complete until September, 2022.

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. Unified In-Space Propulsion Framework for Prediction of Plume-Induced Spacecraft Environments

    SBC: CFD Research Corporation            Topic: T102

    Chemical contamination of spacecraft components as well as thermal and force loading from firing liquid propellant thrusters are critical concerns for in-space propulsion applications. Gas molecular contamination and liquid droplet deposition due to incomplete combustion threaten to damage surface materials, sensitive instruments and optical sensors, and poses major risks for mission success. Liqu ...

    STTR Phase II 2017 National Aeronautics and Space Administration
  2. Active Radiation Shield

    SBC: Gloyer-Taylor Laboratories Inc.            Topic: T301

    In the Phase I effort, Gloyer-Taylor Laboratories LLC (GTL) verified the feasibility of generating power from space particle radiation. This effort successfully demonstrated electrical power production from a particle radiation source using an initial proof-of-concept device. The effort also identified a second approach that has the potential for even better power generation and offers enhanced ...

    STTR Phase II 2017 National Aeronautics and Space Administration
  3. Novel Mixed-mode TCAD-Commercial PDK Integrated Flow for Radiation Hardening By Design

    SBC: CFD Research Corporation            Topic: DTRA16A003

    Cost-effective application of advanced commercial electronics technologies in DoD space systems requires early development of radiation-hardened-by-design (RHBD) techniques, and use of simulations is critical to the efficiency of this process. CFDRC has developed an integrated, mixed-mode simulation approach allowing their NanoTCAD device physics simulator to interface with commercial circuit simu ...

    STTR Phase I 2017 Department of DefenseDefense Threat Reduction Agency
  4. Transient Acoustic Environment Prediction Tool for Launch Vehicles in Motion during Early Lift-Off

    SBC: CFD Research Corporation            Topic: T102

    Launch vehicles experience extreme acoustic loads dominated by rocket exhaust plume interactions with ground structures during lift-off, which can produce damaging vibro-acoustic loads on the vehicle and payloads if not properly understood and mitigated against. Existing capabilities for modeling the turbulent plume physics during early lift-off are too dissipative to accurately resolve the propag ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  5. Multiphase Modeling of Solid Rocket Motor Internal Environment

    SBC: CFD Research Corporation            Topic: T102

    Solid rocket motor (SRM) design requires thorough understanding of the slag accumulation process in order to: predict thrust continuity, optimize propellant conversion efficiency, predict coning effects from sloshing, and assess potential orbital debris (slag) hazard. Current state-of-the-art models for SRM environment do not have the capability to simulate the accumulation and dynamics of slag in ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  6. Launch Weather Decision Support System

    SBC: Radiometrics Corporation            Topic: T103

    Launch safety and efficiency requires timely and accurate wind, thermodynamic and pressure information from the surface to 20 km height, and lightning risk identification. A Doppler radar now provides wind measurements that satisfy this requirement at the Eastern Test Range. Thermodynamic soundings are provided by intermittent radiosondes on launch day. Typical intervals of an hour or more between ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  7. Efficient On-board Lamberts Solution for DSM

    SBC: Advanced Space LLC            Topic: T1102

    Distributed Spacecraft Missions (DSMs) such as constellations, formation-flying missions, and fractionated missions provide unique scientific and programmatic benefits. Distributed mission architectures allow for multipoint in-situ measurements, multi-angle viewpoints, and considerably improved understanding of the connections between separately measured phenomena and their time variations. DSMs a ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  8. Composite Repair System

    SBC: Gloyer-Taylor Laboratories Inc.            Topic: T1202

    GTL has developed an innovative composite repair methodology known as the Composite Repair System (CRS). In this phase I effort, CRS is being developed for the repair of damaged induced in thin-laminate composite cryotanks. In applying CRS to damaged composite structures, the required level of structural capacity is recovered to within a predetermined percentage of its original performance after ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  9. Prediction and Control of Selective Laser Melting Product Microstructure

    SBC: CFD Research Corporation            Topic: T1204

    Despite the rapid commercialization of additive manufacturing technology such as selective laser melting, SLM, there are gaps in models for material microstructure and property prediction that slow qualification and certification. Improvements in coupling microstructure prediction models to local process conditions, validation, and control of material microstructure are required to mature the stat ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  10. Maneuvering Environment for Tiltwing Aircraft with Distributed Electric Propulsion

    SBC: EMBEDDED DYNAMICS LLC            Topic: T1501

    The tiltwing class of aircraft consists of vehicles with the ability to rotate the wing and propulsion system as a unit a full 90 degrees from the standard fixed wing configuration to one in which the wing and thrust axis become perpendicular to the body axis. This thrust vectoring capability allows the aircraft to utilize thrust borne flight for vertical takeoff and landing as well as the convent ...

    STTR Phase I 2017 National Aeronautics and Space Administration
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