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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. 50-kV/1-A Sub-Microsecond Power Switch for Gyrotron Modulation

    SBC: GANIFY LLC            Topic: M

    To enable fast and robust bias modulators for gyrotrons used in the nuclear fusion systems, GaNify LLC will develop a power switch capable of switching 50-kV and 1-A within 1 µs, without the need of series-stacking. This new technology will significantly reduce the circuit complexity and shorten the modulation voltage rise time. The new 50-kV power switch is based upon the demonstrated 10-kV gall ...

    SBIR Phase I 2023 Department of EnergyARPA-E
  2. Attachment of Additively Manufactured RF Windows for Hypersonics

    SBC: MATERIALS RESEARCH & DESIGN INC            Topic: MDA22T011

    Current materials which are available to designers of hypersonic seeker windows are often difficult to manufacture and made in small quantities at significant cost due to the demanding conditions encountered by these materials during hypersonic flight. High temperatures, aerodynamic pressures, and dynamic loading due to maneuvering of hypersonic vehicles produce an extreme thermomechanical environ ...

    STTR Phase I 2023 Department of DefenseMissile Defense Agency
  3. Low Cost Carbon-Carbon Development for Hypersonic Flight Systems-- MSC P4728

    SBC: MATERIALS SCIENCES LLC            Topic: MDA22T013

    Carbon-Carbon (C-C) composites have a thermal protection systems (TPS) pedigree for next generation hypersonic flight systems due their retention of mechanical properties at temperatures exceeding 2,000°C. Continued research and development on C-C composites is required to increase the national capability, capacity, and speed of delivery for C-C composite materials. Innovative low-cost C-C compos ...

    STTR Phase I 2023 Department of DefenseMissile Defense Agency
  4. High-Temperature, Pressure-Activated, Dynamic Seals for Solid Rocket Motors

    SBC: CREARE LLC            Topic: MDA21011

    Future solid propulsion systems will require higher propellant burn temperatures to achieve improvements in impulse and thrust. We propose to continue development of our novel seal technology that will enable significant increases in temperature at the seal location. In Phase I, we proved the feasibility of our approach through analysis, prototyping, and proof‑of‑concept demonstrations. In Pha ...

    SBIR Phase II 2023 Department of DefenseMissile Defense Agency
  5. Predict Signatures of Hypersonic Missiles

    SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC            Topic: MDA21015

    Using Combustion Research’ Flowfield Module (FM) approach, the Phase I effort laid the groundwork for the Hypersonic Vehicle Flowfield Module (HVFM) for axisymmetric/two-dimensional powered hypersonic missiles. As with all our FM tools, HVFM has an Intelligent Automated Architecture (IAA) agent which controls all aspects of the high-fidelity simulation pipeline allowing for non-experts in comput ...

    SBIR Phase II 2023 Department of DefenseMissile Defense Agency
  6. Improved Hypersonic Jet Interaction Modeling with Propulsion Exhaust

    SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC            Topic: MDA22T005

    For hypersonic glide vehicle (HGV) and hypersonic cruise missile (HCM) engagement scenarios intercept occurs in a flight regime where aerodynamic interaction and chemical reacting flow effects are large. To support the development of HGV and HCM intercept vehicle concepts, this program extends a current state-of-the-art hypersonic flow solver and modeling toolkit, Reentry Vehicle Flowfield 3-D Mod ...

    STTR Phase I 2023 Department of DefenseMissile Defense Agency
  7. Engineered Printed Propulsion Technology: A Study on Geometry-Based Thermal Management

    SBC: PLUS DESIGNS INC            Topic: MDA21T005

    Tungsten-based materials such as pure tungsten and tungsten-rhenium alloys are attractive hot-walled material options for solid rocket motor components, but they possess a high thermal diffusivity and can present some design challenges for thermal management. These challenges manifest themselves where geometric constraints, such as small thicknesses/volumes, coupled with long burn times and high t ...

    STTR Phase II 2023 Department of DefenseMissile Defense Agency
  8. High-Temperature, Pressure-Activated, and Infinite-Shelf-Life Dynamic Seals for Solid Rocket Motors

    SBC: CREARE LLC            Topic: MDA21011

    Current dynamic seals in solid rocket motors are limited to relatively low-temperature environments, which limit the compactness and overall temperature capabilities of the motors. We propose to develop a novel seal technology that will enable significant increases in temperature at the seal location, reduce friction and actuation loads, and offer infinite shelf life. In Phase I we will prove the ...

    SBIR Phase I 2022 Department of DefenseMissile Defense Agency
  9. Advanced Vertical Electrodynamic Gradient Freeze System for High-yield CdZnTe Single Crystal Growth

    SBC: NIOUS TECHNOLOGIES INC            Topic: MDA21013

    The goal of the proposed project is to develop an innovative advanced Electrodynamic Vertical Gradient Freeze (VEDGF) crystal growth system with superior performance, versatility, stability, and longevity to produce large single-crystal CdZnTe wafers for long-wave infrared detector arrays. The project is aiming to develop an advanced VEDGF system that offers the following performance and capabilit ...

    SBIR Phase I 2022 Department of DefenseMissile Defense Agency
  10. Predict Signatures of Hypersonic Cruise Missiles

    SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC            Topic: MDA21015

    Our unique position allows us to begin assessing models for hypersonic flow prediction on real-world systems and immediately begin to develop tools that will support acquisition, tracking, and trajectory prediction for hypersonic cruise missiles (HCMs) accomplished largely through signatures electro optical/infrared (EO/IR), radio frequency (RF), radar cross section (RCS) and acoustic. For the Pha ...

    SBIR Phase I 2022 Department of DefenseMissile Defense Agency
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