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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. Advanced Bio-inspired Imaging System with Multiple Optical Sensing Modes

    SBC: SPECTRAL IMAGING LABORATORY            Topic: AF171084

    The U.S. Air Force has a need to develop a new class of advanced, wide field of view (WFOV) imaging system that can sample the radiation field in multiple modes, and with high dynamic range under low-light level viewing conditions. These multimodal systems can be deployed on high altitude drones to enhance their intelligence, surveillance, and reconnaissance (ISR) capabilities. They can also be us ...

    SBIR Phase II 2018 Department of DefenseAir Force
  2. Advanced Dry Cooler for sCO2 Power Systems

    SBC: ALTEX TECHNOLOGIES CORPORATION            Topic: 30f

    As a result of changes in regulations and permitting, the use of water for cooling in nuclear and other utility power plants is being constrained. Dry Coolers have larger footprints and costs, which burdens ratepayers, but achieves the objective of little to no water use. Due to of steam characteristics, Rankine steam cycle power plants have significant cost challenges, when converting to dry cool ...

    SBIR Phase I 2018 Department of Energy
  3. Advanced Electric Motor Technology for Hybrid More Electric/Micro-Turbine Architectures

    SBC: TOYON RESEARCH CORPORATION            Topic: A17002

    There is growing interest in the possibility of turboelectric propulsion for aircraft primarily due to the potential for significant fuel savings. This is enabled by the decoupling of the turbine engine and propulsor. The turbine’s shaft speed can then be optimized for power production while the shaft speed of the propulsor fan can be independently optimized for efficient thrust. Other advantage ...

    SBIR Phase I 2018 Department of DefenseArmy
  4. ADVANCED FIRE CONTROL AUGMENTATION SYSTEM FOR C-UAS

    SBC: Technology Service Corporation            Topic: SOCOM173005

    TSC proposes to combine several high-TRL systems, each performing a key piece of the C-UAS kill chain, into a combined Fire-Control Augmentation System (FCAS) for a SOCOM 40mm weapon system.

    SBIR Phase I 2018 Department of DefenseSpecial Operations Command
  5. Advanced Fire Control Radar for Group 1 and 2 Unmanned Surveillance Systems

    SBC: Physical Optics Corporation            Topic: A17126

    To address the Army’s need for a fire control radar for small UASs, Physical Optics Corporation (POC) proposes to develop an Advanced Fire Control Radar for Group 1 and 2 Unmanned Surveillance Systems (ARGUS). ARGUS is a compact, lightweight, and low power sensor that directly fits in the electronics or payload bay of Group 1 and 2 UASs. It interfaces with the platform’s flight computer throug ...

    SBIR Phase I 2018 Department of DefenseArmy
  6. Advanced High End Gyroscopes for Small Form Factor Inertial Measurement Unit Applications

    SBC: FREEDOM PHOTONICS LLC            Topic: MDA18005

    In this program, Freedom Photonics will develop a novel, miniature gyroscope that meets the requirements of the MDA. This gyroscope will be based on our prior work and demonstration of the gyroscope with similar performance, but larger footprint. Approved for Public Release | 18-MDA-9710 (6 Jul 18)

    SBIR Phase I 2018 Department of DefenseMissile Defense Agency
  7. Advanced High Performance, High Energy Density, Ionic Liquid Propellants for Insensitive Munition Compliant Exo-Atmospheric Interceptors

    SBC: PHYSICAL SCIENCES INC.            Topic: MDA18004

    Physical Sciences Inc. proposes to design, develop and demonstrate a novel insensitive munition compliant, high performance, green storable liquid propellant for advanced exo-atmospheric interceptors. This new propellant formulation can be treated as a monopropellant or as a bipropellant system with predicted specific impulse and density specific impulses exceeding AF-M315E, LMP-103S, and the dens ...

    SBIR Phase I 2018 Department of DefenseMissile Defense Agency
  8. Advanced High Speed Bus Technologies for Units Under Test (UUT), Test and Evaluation

    SBC: A.T.E. SOLUTIONS, INC.            Topic: N162106

    This proposal is for research and development of a methodology for testing high speed input/output signals from avionics line replaceable unit (LRU) in military applications where the military’s automated test equipment (ATE) is from an era prior to the use of signals in the Gbps data rates. A methodology and a novel approach is proposed that not only will supply the necessary stimulus and respo ...

    SBIR Phase II 2018 Department of DefenseNavy
  9. Advanced High Speed Bus Technologies for Units Under Test (UUT), Test and Evaluation

    SBC: Technology Service Corporation            Topic: N162106

    The DoD family of automatic test systems (ATS), primarily interfaces with conventional data buses and is unable to support modern, high-speed digital data buses. Because the latest aircraft avionics and weapons systems are now incorporating high-speed buses such as SATA, IEEE 802.11 WLAN, IEEE 1394 FireWire, and USB, there is an immediate need to integrate high-speed bus testing into DoD ATS. With ...

    SBIR Phase II 2018 Department of DefenseNavy
  10. Advanced Ignition System for Hybrid Rockets for Mars Sample Return, Phase II

    SBC: ULTRAMET            Topic: S4

    To return a sample from the surface of Mars or any of the larger moons in the solar system will require a propulsion system with a comparatively large delta-V capability. Consequently, significant propellant mass will be required. While it is technically feasible to generate O2 and CO propellants by electrolysis of CO2 from the Martian atmosphere, it will only work on bodies where there is signifi ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
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