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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. RF Front End Based on MEMS Components for Miniaturized Digital EVA Radio

    SBC: ALPHASENSE, INC.            Topic: O104

    In this proposal, AlphaSense, Inc. (AI) and the Carnegie Mellon University (CMU) detail the development of RF front end based on MEMS components for miniaturized digital EVA radio. Key innovations of our approach include: a) the use of a novel parallel receiver front end architecture based on MEMS components, b) a novel design of a high Q mixer-filter for RF mixing and IF filtering, and c) the imp ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  2. Rad-hard Location and Attitude Module (R-LAM)

    SBC: Archangel Systems, Inc.            Topic: S402

    R-LAM (Rad-hard Location and Attitude Module), promises a new generation of both integrated navigation modules and stand-alone navigation subsystems including nav-grade IMU's, atomic-precision clocks and GPS units compliant with the Space Plug and Play Architecture (SPA) initiative. R-LAM leverages two active DARPA MTO programs. In the Navigation-Grade Integrated Micro-Gyroscope (NG-IMG) project ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  3. Constant Volume Combustion Engine for Planetary Ascent Vehicles

    SBC: STREAMLINE AUTOMATION LLC            Topic: S308

    The Mars Sample Return mission is being planned to return samples of Martian rock, regolith, and atmosphere to Earth for scientific analysis. The Martian sample size is directly affected by the propulsion capabilities of the Mars Ascent Vehicle (MAV) and innovations are sought to enhance propulsion capabilities of the MAV for functions including primary propulsion from the Mars surface, orbit inse ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  4. A Miniaturized Sensor for Microbial Monitoring of Spacecraft Water Environment

    SBC: CFD RESEARCH CORPORATION            Topic: X203

    Accurate real-time microbial monitoring of water environment is of paramount importance to crew health as well as to ensure proper functioning and control of the life support system during space exploration. The existing methods are time-consuming and labor-intensive, and the devices used are bulky, consumable-hungry, and ill-suited for spacecraft deployment. We propose to develop and demonstrate ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  5. Software for Automated Generation of Reduced Thermal Models for Spacecraft Thermal Control

    SBC: CFD RESEARCH CORPORATION            Topic: S302

    Thermal analysis is increasingly used in thermal engineering of spacecrafts in every stage, including design, test, and ground-operation simulation. Current high-fidelity modeling and simulation tools are computationally prohibitive and not fully compatible to integrated, multi-physics (e.g., thermal-structural-optical) analysis of spacecrafts, particularly in a single model topology currently bei ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  6. Computational Tool for Coupled Simulation of Nonequilibrium Hypersonic Flows with Ablation

    SBC: CFD RESEARCH CORPORATION            Topic: X901

    The goal of this SBIR project is to develop a computational tool with unique predictive capabilities for the aerothermodynamic environment around ablation-cooled hypersonic re-entry vehicles. The framework for this tool will be developed such that all relevant models can be coupled to the LeMANS code for nonequilibrium hypersonic flows and the MOPAR code for ablation material response, both develo ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  7. Improved Design of Radiation Hardened, Wide-Temperature Analog and Mixed-Signal Electronics

    SBC: CFD RESEARCH CORPORATION            Topic: X103

    NASA space exploration projects require avionic systems, components, and controllers that are capable of operating in the extreme temperature and radiation environments of deep space. To design wide-temperature radiation-hardened (rad-hard) electronics and predict characteristics and reliability in space, advanced models and simulation tools are required at multiple levels. Analog and mixed-signal ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  8. Integrated Inflatable Ballute for Planetary Entry

    SBC: CFD RESEARCH CORPORATION            Topic: X902

    CFDRC and TRLA are proposing to develop, design, and test a mass-optimized isotensoid inflatable structure that makes maximum utilization of materials in providing tailored stiffness and rigidity for hypersonic entry vehicles. The proposed inflatable structure is a hybrid isotensoid pressure restraint employing an impervious cloth-reinforced barrier structure enveloped by an integrated array of hi ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  9. GPU-Accelerated Sparse Matrix Solvers for Large-Scale Simulations

    SBC: EM PHOTONICS INC            Topic: S601

    Many large-scale numerical simulations can be broken down into common mathematical routines. While the applications may differ, the need to perform functions such as matrix solves, Fourier transforms, or eigenvalue analysis routinely arise. Consequently, targeting fast, efficient implementations of these methods will benefit a large number of applications. Graphics Processing Units (GPUs) are e ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  10. Nano-Particle Scandate Cathode for Space Communications

    SBC: E BEAM INC            Topic: O107

    We propose an improved cathode based on our novel theory of the role of scandium oxide in enhancing emission in tungsten impregnate cathodes. Recent results have demonstrated the efficacy of nano-particle scandium oxide, but a detailed theory on mechanism has been lacking. Our theory explains published data and point to an optimized cathode which we here propose to build and test at our facility ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
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