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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. Naval Platform Aero-Optic Turbulence and Mitigation Methodology

    SBC: MZA ASSOCIATES CORP            Topic: N13AT001

    MZA partnered with the University of Notre Dame proposes to transition the Navys HEFL Beam Director Subsystem (HBDS) for flight testing on the Airborne Aero-Optics Laboratory Transonic (AAOL-T) aircraft. We will reconfigure the HBDS integrating structure and aft beam control system to fit the cabin constraints of the AAOL-T aircraft with an aft beam control and scoring bench. Operational functiona ...

    STTR Phase II 2016 Department of DefenseNavy
  2. Compact Megavolt Switch Utilizing Novel Switching Mediums

    SBC: ASR Corporation            Topic: N14AT018

    The Navy has a need to control such extreme power specifications that no suitable switches exist. The Navy power specifications require us to develop a novel medium (probably a pressurized gas or liquid) that can be configured to meet the requirements and control the flow of electrical power directly. Our extensive switching expertise has allowed us to develop a series of novel test fixtures and t ...

    STTR Phase II 2016 Department of DefenseNavy
  3. Revolutionary Airlift Innovation

    SBC: LOGISTIC GLIDERS INC.            Topic: ST14B004

    We propose to mature LG-X glider technology by manufacturing full-scaled prototypes and characterizing them in land-based flight-testing by using commercial aircraft to drop the gliders. Validated components such as the landing parachute, folding wing mechanism, and autopilot control system will undergo integrated flight-testing. Logistic Gliders will provide a considerable cost share to support ...

    STTR Phase II 2016 Department of DefenseDefense Advanced Research Projects Agency
  4. Data Driven Intent Recognition Framework

    SBC: OTHER LAB, INC.            Topic: NSF13599

    A critical aspect of exoskeleton control that has to date introduced a performance limitation is the ability of the exoskeleton to recognize the intent of the operator so it can apply assistance to their desired motion. This intent recognition effort is typically solved using ad-hoc methods where subject matter experts make design decisions and tune transitions to identify intended maneuvers as re ...

    STTR Phase II 2016 Department of DefenseSpecial Operations Command
  5. Decision Making under Uncertainty

    SBC: GCAS, Inc.            Topic: MDA13T001

    Our proposed second order uncertainty (SOU) product is a decision making software solution that addresses the problem of providing accurate and precisely defined decision courses of action (COAs) of complex, time-constrained problems in a fraction of the time required by alternative methods striving to achieve the same level of precision. Complex decision situations can deal with large volume of ...

    STTR Phase II 2016 Department of DefenseMissile Defense Agency
  6. High Gain, High Power PCSS with Integrated Monolithic Optical Trigger

    SBC: Eureka Aerospace            Topic: A14AT004

    This proposal addresses the problem of PCSS/laser trigger integration using a single monolithic laser diode array, thus simplifying the entire optical delivery network necessary for efficient operation of PCSSs. The proposal constitutes a logical continuation of Phase I effort where the main focus was on the detailed design of the PCSS/laser diode array (LDA) integrated architecture. In Phase II ...

    STTR Phase II 2016 Department of DefenseArmy
  7. High Fidelity Rotorcraft Towing Modeling and Simulation with Towed Magnetic Anomaly Detection System

    SBC: ADVANCED ROTORCRAFT TECHNOLOGY, INC.            Topic: N15AT009

    Towing of a Magnetic Anomaly Detection (MAD) system is an important aspect of rotorcraftmaritime operation. The oscillatory rotorcraft combined with the long and flexible towingcable, the low mass ratio of the towed body to the towing aircraft, and the rotor wake effecton the towed body presents a challenge for integration of a modern MAD system withrotorcraft platform. The research objective is t ...

    STTR Phase II 2016 Department of DefenseNavy
  8. 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
  9. Lightweight, Stable Optical Bench with Integrated Vibration Attenuation

    SBC: SAN DIEGO COMPOSITES, INC.            Topic: MDA13T007

    The goal of this program is to design a lightweight optical bench capable of remaining stable under temperature and moisture changes, while isolating the precision optical array from vibrations such as engine noise and air turbulence. By integrating a customizable periodic stack in the bench, vibrations are attenuated more effectively than commercially available mounts. Additionally, the periodic ...

    STTR Phase II 2016 Department of DefenseMissile Defense Agency
  10. Rotorcraft External Far-Field Noise Measurement Using a Hot-Air Balloon

    SBC: DELTA GROUP INTERNATIONAL LLC            Topic: A14AT001

    An innovative and fundamental approach to measure far field noise of a helicopter using a hot-air balloon as an acoustic measurement platform is described. The technique, featuring a microphone suspended beneath the basket of a hot-air balloon, is used to obtain acoustic data above, in, and below the horizon plane of a helicopter in forward flight. This approach is postulated to have many advantag ...

    STTR Phase II 2016 Department of DefenseArmy
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