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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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. Automated Detection of Steganographic Content

    SBC: COLORADO ENGINEERING INC.            Topic: AF04T008

    Colorado Engineering, Inc., a small woman owned business, and the University of Colorado at Colorado Springs are teaming to extend a steganogrpahic architecture for an extensible, distributed application that can be utilized to detect steganographic content in media files, alert the user, and either mitigate (destroy) the content if possible or quarantine the files as appropriate. The initial arc ...

    STTR Phase II 2006 Department of DefenseAir Force
  2. TEMBO® Foam for Morphing Wing Applications

    SBC: COMPOSITE TECHNOLOGY DEVELOPMENT, INC.            Topic: AF06T013

    In recent years there has been significant interest in developing morphing air vehicles that would be able to fly efficiently over a wide range of flight regimes to meet new mission profiles. Though morphing-wing concepts have been around for many years, it has been determined that conventional designs such as swing wings are not adequate for providing the desired improvements. Many of the new m ...

    STTR Phase I 2006 Department of DefenseAir Force
  3. Adaptive Materials for Morphing Aircraft Skins

    SBC: COMPOSITE TECHNOLOGY DEVELOPMENT, INC.            Topic: AF06T017

    In the proposed Phase I program, Composite Technology Development Inc. (CTD) will work with Raytheon Missile Systems to define material requirements for morphing aircraft skins, and will perform material evaluations to demonstrate the feasibility of adaptive materials with dynamically variable stiffness. Georgia Tech Research Corporation (GTRC) will provide mechanical characterization support.

    STTR Phase I 2006 Department of DefenseAir Force
  4. Combustion Stability Innovations for Liquid Rocket Engines

    SBC: IN SPACE, L.L.C.            Topic: AF06T005

    While guidelines for stable combustion in certain engine cycles and propellant combinations exist; there is no proven, mechanistic predictive model, particularly for high-performance liquid hydrocarbon-fueled engines. IN Space and Purdue propose to fill this critical need by developing a “testbed” consisting of 1) a predictive combustion stability design tool to mitigate the risk of generating ...

    STTR Phase I 2006 Department of DefenseAir Force
  5. MINIATURIZED ELECTRO/MAGNETO-OPTIC SENSORS FOR THE DETECTION AND MEASUREMENT OF BROADBAND RF PULSES

    SBC: Opteos, Inc.            Topic: AF04T025

    An innovative, high-speed electromagnetic-wave-detection system based on broadband, non-intrusive, miniaturized electro-optic (EO), magneto-optic (MO), and electro-optic voltage (EOV) sensors will be developed for evaluating the effects that pulsed electromagnetic (EM) waves have on specific components of electronic systems. The suite of optically-interrogated sensors, which may be positioned with ...

    STTR Phase II 2006 Department of DefenseAir Force
  6. Soluble Catalysts to Improve Jet Fuel Combustion and Fuel Heat Sink Capacity

    SBC: TDA RESEARCH, INC.            Topic: AF06T019

    Rocket Based Combined Cycle (RBCC) propulsion systems likely will be used to launch next-generation space vehicles. However, in the scramjet portion of the cycle, it is difficult to maintain stable combustion because of the high air velocity and short combustor residence times. In addition, the overall heat load in a scramjet engine exceeds the cooling capacity that can be provided from the sens ...

    STTR Phase I 2006 Department of DefenseAir Force
  7. Kinetic Mechanisms for Reacting Flow CFD

    SBC: REACTION SYSTEMS, INC.            Topic: OSD05T002

    Development of scramjet engines is hindered by the lack of fast and accurate turbulent reacting flow CFD tools. In Phase I of this STTR project, Reaction Systems, LLC investigated a fundamentally new approach to reducing the computational burden of detailed chemistry that holds great promise in lowering this computational burden. This new approach significantly reduces the number of chemical spe ...

    STTR Phase II 2006 Department of DefenseAir Force
  8. Triple3 Redundant Spacecraft Subsystems (T3RSS)

    SBC: REDEFINE TECHNOLOGIES, INC.            Topic: T101

    Redefine Technologies, along with researchers at the University of Colorado, will use three redundancy methods to decrease the susceptibility of a spacecraft, on a mission survivability level, to electronic failures anywhere throughout the spacecraft. By using Field Programmable Gate Array (FPGA) chips, we will analyze the spacecraft-wide benefits of: *triplicating the logic and RAM on-board eac ...

    STTR Phase I 2006 National Aeronautics and Space Administration
  9. Nanodielectrics for High Power Capacitors and Passive Applications

    SBC: SYNKERA TECHNOLOGIES INC            Topic: AF06T002

    This Small Business Technology Transfer Phase I project seeks to develop and commercialize novel nanodielectrics with the internal structure enabling extremely high values of the dielectric constant. Lightweight, compact, high energy density capacitors capable of operation at several MJ per pulse and repetition rates on the order of 100 pps bursts are needed for directed energy weapons. High alt ...

    STTR Phase I 2006 Department of DefenseAir Force
  10. Nanocatalysts for Hydrocarbon-Fueled Rocket Based Combined Cycle (RBCC) Engines

    SBC: SYNKERA TECHNOLOGIES INC            Topic: AF06T019

    This Small Business Innovation Research Phase I project involves the development of homogeneous catalysts for cracking of hydrocarbon fuel. Future concept space vehicles employ regeneratively cooled engines which rely on the fuel to absorb engine heat to ensure survival of the engine structure at a high temperature. Using the fuel to absorb heat and burning the hot fuel efficiently keeps the heat ...

    STTR Phase I 2006 Department of DefenseAir Force
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