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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

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. Smart Tooling for Manufacturing Composites

    SBC: CORNERSTONE RESEARCH GROUP INC            Topic: X503

    CRG's shape memory polymer (SMP) tooling technologies, Smart Tooling, offer cutting-edge manufacturing solutions that can meet the construction needs of all future composite platforms and systems. Development and implementation of Smart Tooling, Smart Mandrels and SMP Bladders, offers end users significant opportunities to save direct expense for tooling cost and manufacturing labor to fabricate c ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  2. Integrated Sublimator Driven Coldplate for use in Active Thermal Control System

    SBC: PARAGON SPACE DEVELOPMENT CORPORATION            Topic: X205

    The original Sublimator Driven Coldplate (SDC) design sought to provide significant mass savings over a traditional pumped fluid loop by combining the functions of a cold plate and a sublimator and eliminating the fluid loop (Leimkuehler, et. al., "Design of a Sublimator Driven Coldplate Development Unit," 2008-01-2169). The target application was to provide heat rejection for the ascent module of ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  3. Aircraft Engine Life-Consumption Monitoring for Real-Time Reliability Determination

    SBC: Nastec, Inc.            Topic: A108

    The object of this research is to develop an in-service life-monitor system for the prediction of the remaining component and system life of aircraft engines. The embedded system will monitor the engines thrust, exhaust gas temperature, the engine efficiency, the speed and the time of operation of the engine in flight. Based upon this data, the life-estimation analog of the system will calculate ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  4. Unconditionally Stable Low Dropout Regulators for Extreme Environments

    SBC: SJT Micropower            Topic: X103

    We have developed a low dropout (LDO) regulator using a patented MESFET transistor technology that can be manufactured in commercial CMOS foundries with no changes to the process flow. The regulator is stable under all load conditions without an external compensation capacitor, thereby reducing the mass/volume of the power management system and increasing reliability. The MESFET-based LDO componen ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. Low Mass Electromagnetic Plasmoid Thruster with Integrated PPU

    SBC: MSNW LLC            Topic: S304

    The Electromagnetic Plasmoid Thruster (EMPT) is a revolutionary electric propulsion thruster and power processing (PPU) system that will allow a dramatic decrease in system mass and increase in thrust efficiency over traditional 500-3000 W propulsion systems. The high specific power (>700 W/kg) and high efficiency of EMPT will enable a wide range of deep space missions such as Neptune, Pluto and O ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  6. RF Front End Based on MEMS Components for Miniaturized Digital EVA Radio

    SBC: ALPHASENSE, INC.            Topic: O104

    In this SBIR project, AlphaSense, Inc. and the Carnegie Mellon University propose to develop a RF receiver front end based on CMOS-MEMS components for miniaturized digital EVA radio applications. In Phase I, we have proven the feasibility of implementing a compact, low power and high performance S band receiver front end based on CMOS- MEMS components. Specifically, we conducted link budget analys ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  7. Improved Metal-Polymeric Laminate Radiation Shielding

    SBC: POWDERMET INC            Topic: X401

    In this proposed Phase II program, builds on the phase I feaibility where a multifunctional lightweight radiation shield composite was developed and fabricated. This structural radiation shielding is high strength, syntactic polymeric where the polymer is filled with high strength low Z material. The phase II program will provide radiation modeling and testing for these new structural radiation s ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  8. On-Line Flutter Prediction Tool for Wind Tunnel Flutter Testing using Parameter Varying Estimation Methodology

    SBC: ZONA TECHNOLOGY INC            Topic: A204

    ZONA Technology, Inc. (ZONA) proposes to develop an on-line flutter prediction tool using the parameter varying estimation (PVE) methodology, called the PVE Toolbox, to ensure the flight safety during the flight flutter test and to prevent the damage to the wind tunnel hardware from the structural failure of the flutter model during wind tunnel flutter test. This tool can be applied to rapidly ide ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  9. Flight Dynamic Simulation with Nonlinear Aeroelastic Interaction using the ROM-ROM Procedure

    SBC: ZONA TECHNOLOGY INC            Topic: A207

    ZONA Technology, Inc. proposes to develop an integrated flight dynamics simulation capability with nonlinear aeroelastic interactions by combining a flight dynamics model and an add-on nonlinear aeroelastic solver in a Simulink environment. This nonlinear aeroelastic solver is generated by interacting a nonlinear structural Reduced Order Model (ROM) with a Neural-Network-based (NN-based) aerodyna ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  10. Wide Temperature Rad-Hard ASIC for Process Control of a Fuel Cell System

    SBC: RIDGETOP GROUP INC            Topic: X103

    Ridgetop Group developed a top-level design of a rad-hard application-specific integrated circuit (ASIC) for spacecraft power management that is functional over a temperature range of -180 to +130oC. This ASIC is intended to work in conjunction with a fuel cell power system and battery backup to provide uninterrupted power to critical modules in space.Ridgetop has designed a novel integ ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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