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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

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. 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
  3. 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
  4. 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
  5. Air Vehicle Gust Response analysis for Conceptual Design

    SBC: Research In Flight, LLC            Topic: T15

    Research in Flight (RIF) and Auburn University are offering the development of an advanced, robust tool and methodology that allows the simulation and modeling of gust and wake vortex encounters for Distributed Electric Propulsion (DEP) enabled Urban Air Mobility (UAM) vehicle concepts. DEP enabled UAM concepts offer the potential for large performance improvements by exploiting favorable synergie ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  6. A Modular In-Situ Curing Apparatus for Thermoset Resin Mixtures Applied as Thermal Protection Systems

    SBC: Intelligent Optical Systems, Inc.            Topic: T12

    Future human extraterrestrial missions will require export and landing of countless payloads on the lunar and Martian surfaces. Such a quantity and rate of payload delivery will require cost-effective and rapid manufacturing of many large Thermal Protection Systems (TPS). IOS proposes to develop a modular system for in-situ bonding and curing of thermoset resin to the spacecraft structure to facil ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  7. 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
  8. 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
  9. A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin

    SBC: REACTION SYSTEMS, INC            Topic: T6

    Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  10. Attitude Control Enhancement Using Distributed Wing Load Sensing for Dynamic Servoelastic Control

    SBC: Systems Technology, Inc.            Topic: T402

    Fly-by-feel uses distributed sensing of forces along the lifting surfaces of an aircraft. Whether such measurements are made via hot films, pressure sensors, or strain gauges, all can provide distributed force information that must be intelligently fused and utilized to achieve performance goals. Fly-by-feel will be used to achieve robust disturbance rejection, mass property augmentation, and aero ...

    STTR Phase I 2013 National Aeronautics and Space Administration
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