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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. SmallSat Stirling Cryocooler for BMDS (SSC-X)

    SBC: WECOSO, INC.            Topic: MDA17T003

    West Coast Solutions (WCS) proposes the development of the SSC-X Stirling cryocooler to enable the deployment of infrared (IR) payloads on small satellite platforms. We achieve extreme miniaturization (

    STTR Phase II 2019 Department of DefenseMissile Defense Agency
  2. Conformal Aerodynamic Controls for Supermaneuverable High-Speed Vehicles

    SBC: ATA ENGINEERING, INC.            Topic: MDA18T002

    High G Aerodynamic Controls | Approved for Public Release 18-MDA-9707 (3 Jul 18)

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  3. Low Toxicity, Non-cryogenic Liquid Propellant Upper Stage Engine

    SBC: Science and Technology Applications, LLC            Topic: MDA18T005

    Our vision for the next generation missile and space propulsion engine is a flexible and non-toxic propulsion technology using HAN/kerosene, offering variable thrust with a high degree of mission tailoring. Additionally, high bulk density of HAN/kerosene bi-propellant improves stage mass fraction and delivers performance metrics that exceed current toxic storable propellants. We propose an innovat ...

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  4. Equester Green Propellant Turbopump

    SBC: EXQUADRUM INC            Topic: MDA18T005

    During the proposed Phase 1 research and development effort, the project team will design an innovative turbopump system for a target vehicle upper stage using “Green" liquid propellants that meet Missile Defense Agency's requirements. The use of a turbopump will result in an upper stage that has a greater than 50% improvement in delta velocity in comparison to a previously designed, pressure fe ...

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  5. Storable Clean Ethane/ethylene Nitrous Engine (SCENE)

    SBC: PIONEER ASTRONAUTICS            Topic: MDA18T005

    he Storable Clean Ethane-ethylene Nitrous Engine (SCENE) is a proposed technology designed to provide upper stages and spacecraft with non-toxic, liquid, non-cryogenic, high-performance propulsion with an Isp on the order of 300 seconds. The propellant components are stored as liquids under their saturated vapor pressures. With the SCENE, nitrous oxide is used as an autogenously pressurized oxidiz ...

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  6. Non-Intrusive Uncertainty Identification and Quantification Framework for Hypersonic Flights

    SBC: CFD RESEARCH CORPORATION            Topic: MDA18T006

    Uncertainty Reduction in High Speed Flight Vehicle Modeling | Approved for Public Release 18-MDA-9707 (3 Jul 18)

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  7. Uncertainty Reduction in High Speed Flight Vehicle Modeling

    SBC: M4 ENGINEERING, INC.            Topic: MDA18T006

    Uncertainty Reduction in High Speed Flight Vehicle Modeling | Approved for Public Release 18-MDA-9707 (3 Jul 18)

    STTR Phase I 2019 Department of DefenseMissile Defense Agency
  8. Retrofittable and Transparent Super-Insulator for Single-Pane Windows

    SBC: NANOSD, INC.            Topic: DEFOA0001429

    NanoSD, Inc. with its partners will develop a transparent, nanostructured thermally insulating film that can be applied to existing single-pane windows to reduce heat loss. To produce the nanostructured film, the team will create hollow ceramic or polymer nanobubbles and consolidate them into a dense lattice structure using heat and compression. Because it is mostly air, the resulting nanobubble s ...

    STTR Phase II 2016 Department of EnergyARPA-E
  9. Enhancement of Ballistic Missile Defense System Level Simulation Operations Through Multi-core Processing

    SBC: ISSAC Corp            Topic: MDA13T003

    The ISSAC Team propose a novel method to encapsulate legacy models and simulations that allows these components to take advantage of modern, multi-core, multi-processor hardware suites. Encapsulating these legacy codes provides 3 primary advantages to deal with complex systems and systems of systems (Air Force, Navy, Department of Homeland Security (DHS), Federal Emergency Management Agency (FEMA) ...

    STTR Phase II 2016 Department of DefenseMissile Defense Agency
  10. Microelectronics Component Adhesive Selection and Design Rules for Failure Avoidance

    SBC: CFD RESEARCH CORPORATION            Topic: MDA14T002

    Thermally induced fatigue and residual stress introduced during fabrication are sources of failure in microelectronics, which raises reliability concerns for MDA and its system integrators. CFDRC has teamed with experts in the reliability of microelectronics packaging to develop a physics based modeling and testing protocol to correlate material properties and thermal loading conditions to stress ...

    STTR Phase II 2016 Department of DefenseMissile Defense Agency
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