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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. Additive Manufacture of Refractory Metal Propulsion Components

    SBC: Geoplasma, LLC            Topic: T9

    Niobium alloy (C-103) reaction control system (RCS) chambers have been used on numerous NASA programs. However at elevated temperatures, the strength of C-103 decreases significantly. Higher strength niobium alloys have been developed, but these alloys lack the formability of C-103. Recently, Additive Manufacture (AM) of niobium and C-103 has been demonstrated using powder bed electron beam me ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  2. Additive Manufacturing Sensor Fusion Technologies for Process Monitoring and Control.

    SBC: ARCTOS Technology Solutions, LLC            Topic: DLA18A001

    Universal Technology Corporation (UTC) has teamed with the University of Dayton Research Institute (UDRI), Stratonics, and Macy Consulting to demonstrate not only the transitionability into commercial systems, but also to develop the data analytics and monitoring and control requirements to extract the full value fromseveral sensors, including the Stratonics ThermaViz, acoustic and profilometry se ...

    STTR Phase I 2018 Department of DefenseDefense Logistics Agency
  3. Advanced Li/CFx Primary Batteries with Non-Flammable Electrolytes

    SBC: CFX BATTERY, INC.            Topic: T601

    NASA seeks to develop high specific energy primary batteries that are safe and capable of performing under a wide temperature range, for manned space missions. To meet this goal, CFX Battery Inc. proposes to develop, characterize, and establish technological feasibility of a new Li/SF-CFx based high capacity lithium primary battery that offers higher rate capability and enhanced safety than conven ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  4. 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
  5. Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization

    SBC: AMERICAN GNC CORPORATION            Topic: T1

    In providing an innovative solution to improving information technologies and health management systems, AGNC is proposing a significant technological achievement with the Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization. During in-flight conditions, this system is able to not only provide the status of information such as regarding the flight envel ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  6. Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems

    SBC: STREAMLINE NUMERICS, INC.            Topic: T901

    The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a pr ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  7. An Additive Manufacturing Technique for the Production of Electronic Circuits

    SBC: MORNINGBIRD MEDIA CORPORATION            Topic: T12

    Under the support of a FY 2016 NASA Phase I Small Business Technology Transfer (STTR) contract (NASA contract number NNX16CM40P), Morningbird Media Corporation in collaboration with Alabama A&M University Research, Innovation in Science and Engineering (AAMU-RISE) Foundation, has devised a unique method for an additive manufacturing technique for the direct 3D printing of functional electronics. T ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  8. An LED-Based Solar Simulator for Research, Development, and Testing of Photovoltaic Space Power Systems

    SBC: Angstrom Designs, Inc.            Topic: T201

    Solar cells are the critical power source for the majority of space missions. The advancement from single junction silicon cells to current, state-of-the-art, triple junction, germanium cells enabled greater mission power per weight, stowed volume and deployed area. Near-term, advanced solar cell technologies will range from 4 to 6 junctions, and include a variety of band gaps.Solar cell testing ...

    STTR Phase I 2013 National Aeronautics and Space Administration
  9. A Reusable, Oxidizer-Cooled, Hybrid Aerospike Rocket Motor for Flight Test

    SBC: ROLLING HILLS RESEARCH CORP            Topic: T202

    The proposed innovation is to use the refrigerant capabilities of nitrous oxide (N2O) to provide the cooling required for reusable operation of an aerospike nozzle in conjunction with an N2O-HTPB (hydroxyl-terminated polybutadiene, a synthetic rubber that is used as a binder in solid rocket motors and as a fuel in hybrid rocket motors) hybrid rocket motor. The phase change cooling as liquid N2O i ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  10. A Scalable Gas-Particle Flow Simulation Tool for Lander Plume-Surface Interaction and Debris Prediction

    SBC: CFD Research Corporation            Topic: T9

    Spacecraft propulsive landings on unprepared regolith present in extra-terrestrial environments pose a high risk for space exploration missions. Plume/regolith interaction results in (1) the liberation of dust and debris particles that may collide with the landing vehicle and (2) craters whose shape itself can influence vehicle dynamics. To investigate such gas-granular interactions for large-scal ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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