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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. Technologies for Rare Earths Enrichment of a Novel Low-Cost Raw Material

    SBC: PHYSICAL SCIENCES INC.            Topic: OSD12T01

    A critical step in the extraction of elements from ore, especially rare earth elements that are found in complex minerals, is separation. Froth flotation is a highly versatile method for physically separating particles based on differences in the ability of air bubbles to selectively adhere to specific mineral surfaces in a mineral/water slurry. The particles with attached air bubbles are then ca ...

    STTR Phase II 2015 Department of DefenseOffice of the Secretary of Defense
  2. Information Salience

    SBC: DISCERNING TECHNOLOGIES, LLC            Topic: OSD11TD1

    Empirical-based mathematical framework and computer algorithms, for representing human perception and cognition processes and limitations, which influence the recognition of salient information about rapidly changing events.

    STTR Phase II 2015 Department of DefenseOffice of the Secretary of Defense
  3. Recovery of Rhenium from Superalloy Scrap

    SBC: LYNNTECH INC.            Topic: OSD12T04

    Due to the limited amount of rhenium present in the earths crust (approximately 1-2 part per billion) there is a significant benefit to be realized in recovering for reuse the rhenium from scrap material, spent catalysts, or end-of-life superalloys. Rhenium is found in molybdenum-copper porphyry deposits. If rhenium is present in ore that is processed, it will show up in the resulting molybdenum ...

    STTR Phase II 2015 Department of DefenseOffice of the Secretary of Defense
  4. An End-To-End Microfluidic Platform for Engineering Life Supporting Microbes in Space Exploration Missions

    SBC: HJ SCIENCE & TECHNOLOGY INC            Topic: T601

    HJ Science & Technology (HJS&T) and Lawrence Berkeley National Laboratory (LBNL) propose a highly integrated, programmable, and miniaturized microfluidic automation platform capable of running rapid and complex synthetic biology and bioengineering processes for engineering life supporting microbes in space exploration missions. Our approach combines the microfluidic automation technology of HJS&T ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  5. Adaptive Resource Estimation and Visualization for Planning Robotic Missions

    SBC: Traclabs Inc.            Topic: T1101

    NASA's future human exploration missions will include remotely operated rovers performing surface exploration and science, as well as free-flyers to reduce the need for human Extra Vehicular Activity (EVA). As astronauts move deeper into space, it will be necessary for them to manage these robotic assets with less support from ground controllers. A flexible approach is needed to build and revise p ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  6. Fully Printed Flexible 4-bit 2D (4x4) 16-Element Graphene-Based Phased Array Antenna System

    SBC: OMEGA OPTICS, INC.            Topic: T501

    Communication technologies support all NASA space missions, among which autonomous communication technologies are extremely beneficial to future missions, including the Asteroid Redirect Mission, and human expedition to Mars and beyond. Low-cost, high gain, light-weight, and flexible active antenna systems are highly desired. In this program, we propose to develop a fully flexible ink-jet printed ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  7. In-Situ EBCs for High Performance Composite Propulsion Components

    SBC: PHYSICAL SCIENCES INC.            Topic: T1202

    Silicon Carbide based ceramic matrix composites (CMCs) offer the potential to fundamentally change the design and manufacture of aeronautical and space propulsion systems to significantly increase performance and fuel efficiency over current metal-based designs. Physical Sciences Inc. (PSI) and our team members at the University of California Santa Barbara (UCSB) are developing, designing and fabr ...

    STTR Phase II 2015 National Aeronautics and Space Administration
  8. Integrated Reacting Fluid Dynamics and Predictive Materials Degradation Models for Propulsion System Conditions

    SBC: CFD RESEARCH CORPORATION            Topic: T1202

    Computational fluid dynamics (CFD) simulations are routinely used by NASA to optimize the design of propulsion systems. Current methods for CFD modeling rely on general materials properties to determine fluid structure interactions. This introduces uncertainty when modeling extreme conditions, where materials degrade and properties may change as a consequence. This also limits the use of CFD as a ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  9. Sensing Aware Autonomous Communications System

    SBC: Space Micro Inc.            Topic: T501

    Space Micro and its partner research institution, the University of Arizona bring together innovations in channelization and network protocol development. Together, these innovations will provide improved hopping radios (with digital, rapidly reconfigurable implementation, wider bandwidth and reduced overhead penalty for hopping) and improved spectrum and link quality sensing. We will demonstrate ...

    STTR Phase I 2015 National Aeronautics and Space Administration
  10. Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts

    SBC: Tao Of Systems Integration Inc            Topic: T401

    Control of extremely lightweight, long endurance aircraft poses a challenging aeroservoelastic (ASE) problem due to significantly increased flexibility, and aerodynamic, structural, and actuator nonlinearities. To obtain the benefits of increased aerostructural efficiency, the controller needs to trim at a specified optimal shape while minimizing structural fatigue from gust disturbances. Tao Syst ...

    STTR Phase II 2015 National Aeronautics and Space Administration
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