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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. GPU-Accelerated Sparse Matrix Solvers for Large-Scale Simulations

    SBC: EM PHOTONICS INC            Topic: S601

    At the heart of scientific computing and numerical analysis are linear algebra solvers. In scientific computing, the focus is on the partial differential equations (PDEs) that arise from computational fluid dynamics (CFD), climate modeling, astrophysics, and structural and heat analysis that cannot be solved analytically. Certain problem formulations lead to sparse matrices, in which the majority ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  2. 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
  3. Novel Active Combustion Control Concept for High-Frequency Modulation of Atomized Fuel Flow

    SBC: JANSEN'S AIRCRAFT SYSTEMS CONTROLS, INC.            Topic: A202

    This proposal by Jansen's Aircraft Systems Controls, Inc. presents an innovative solution for Active Combustion Control.Relative to the state of the art, this concept has the ability to provide frequency modulation (greater than 1000[Hz]) in combination with high amplitude modulation (in excess of 30% flow) and can be adapted to a large range of fuel injector sizes. Existing state-of-the-art ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  4. High Power Room Temperature Terahertz Local Oscillator

    SBC: Desert Beam Technologies, LLC            Topic: S104

    The motivation of the proposed SBIR is to develop, demonstrate and commercialize a compact, low-mass, high output power (1-10 milliwatt), tunable source of CW THz radiation operating at room temperature. The source will be useful both as a narrow band frequency stable sources for driving heterodyne receivers at key frequencies between 1 and 5 THz (1.4, 1.9, 2.7, 4.7 etc..) or for laboratory source ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. 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
  6. Nonventing Thermal and Humidity Control for EVA Suits

    SBC: CREARE LLC            Topic: X205

    Future manned space exploration missions will require space suits with capabilities beyond the current state of the art. Portable Life Support Systems for these future space suits face daunting challenges, since they must maintain healthy and comfortable conditions inside the suit for long-duration missions while minimizing weight and venting no consumables. We propose to develop an innovative s ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  7. 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
  8. Contaminant Robust System for Oxygen Production from Lunar and Martian Resources

    SBC: PARAGON SPACE DEVELOPMENT CORPORATION            Topic: X301

    Extended duration missions to the Moon and Mars will require the use of In-situ resources to generate propellants and life support consumables. Many of the processes for in-situ resource utilization (ISRU) produce water, along with a variety of acid gases and other water soluble contaminants. Paragon proposes to develop membrane technology to separate water vapor from contaminants in the ISRU sy ...

    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. High Power Narrow Linewidth 1.26 Micron Ho-Doped Fiber Amplifier

    SBC: N.P. PHOTONICS, INC.            Topic: S101

    This proposal is for the development of an innovative, high power, and extremely reliable 1.26-micron Ho-doped fluoride fiber amplifier. The proposed fiber amplifier consists of a Ho-doped fluoride fiber pre-amplifier and power amplifier. Laser at 1187 nm will be used as a resonant pump laser source for Ho3+-doped fiber laser. High gain per unit length at 1.2 micron can be achieved in Ho-doped f ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
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