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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. Extreme Wear-Resistant Thermal Spray Coatings.

    SBC: PLASMA TECHNOLOGY, INC.            Topic: AF09BT19

    The demand for higher performance and rapid transition of new technologies into extreme performance has lead to the need for engineered materials and surface modification technologies. The present proposal is focused on finding a surface engineered solution that can withstand exceptionally harsh environments such as those found in supersonic ground test tracks or rail gun environments. This SBIR p ...

    STTR Phase I 2010 Department of DefenseAir Force
  2. Theoretical Innovations in Combining Analytical, Experimental, and Computational Combustion Stability Analysis

    SBC: METACOMP TECHNOLOGIES INC            Topic: AF09BT38

    The occurrence of combustion instability has long been a matter of serious concern in the development of liquid-propellant rocket engines due to the high rate of energy release in a confined volume in which energy losses are relatively small. Shear layer instabilities and intermittent growth rates of the mixing layer cause fluctuations in the burning rates and result in acoustic waves triggering ...

    STTR Phase I 2010 Department of DefenseAir Force
  3. High Temperature Metal RubberTM Sensors For Skin Friction Measurements

    SBC: NANOSONIC INC.            Topic: AF09BT32

    The Air Force Phase I STTR program would develop and demonstrate high temperature version of ‘sensor skins’ capable of multi-axis flow characterization on air breathing hypersonic engines. This would build upon NanoSonic’s successful demonstration of Metal Rubber™ transducer materials for the measurement of flow-induced skin friction and pressure at low temperatures and transonic and super ...

    STTR Phase I 2010 Department of DefenseAir Force
  4. Coupled Cluster Theory (CCT)

    SBC: DECISIVE ANALYTICS CORPORATION            Topic: AF09BT40

    Single-reference coupled cluster (SRCC) methods have revolutionized our ability to accurately predict molecular energies and properties. As new developments in theory and computer science extend the application of SRCC methods to larger and larger systems, advancements in coupled cluster methods for studying multi-reference systems have lagged far behind. DECISIVE ANALYTICS Corporation has teame ...

    STTR Phase I 2010 Department of DefenseAir Force
  5. Instrumentation for hypersonic, air-breathing engines

    SBC: LUNA INNOVATIONS INCORPORATED            Topic: AF09BT32

    Luna Innovations Incorporated and CURBC (Calspan – University of Buffalo Research Center) are proposing to develop miniature, high-speed, high-temperature, fiber-optic pressure sensors that will fill the void that currently exists between ground and flight test instrumentation. The sensors small size (ø 0.007”) and high-sensitivity (better than ±0.01 psi) combined with a high-speed fiber-op ...

    STTR Phase I 2010 Department of DefenseAir Force
  6. Thermoelectric material-coated carbon nanotubes as high conductivity thermal interface materials

    SBC: ADA TECHNOLOGIES, INC.            Topic: AF09BT22

    The ever-decreasing size of the electronic microchips and the ever-increasing density of electronic components required to support future Air Force platforms are creating the problem of substantial localized heat generation that can impair component operation. State of the art thermal interface materials (TIMs), that are used to dissipate heat from the source to the spreader in a microchip, are se ...

    STTR Phase I 2010 Department of DefenseAir Force
  7. Innovative CFD Algorithm, Libraries & Python Frameworks for Hybrid-GPU Computing Architectures

    SBC: JMSI, INC            Topic: AF09BT18

    The need for faster highly resolved solutions coupled with the advent of General Purpose Graphics Processing Unit (GPGPU) architectures and the development of GPGPU algorithms at the University of California, Davis present an opportunity that JMSI Inc. proposes to leverage by developing algorithmic and software solutions for GPGPUs in “Innovative CFD Algorithms, Libraries & Python Frameworks for ...

    STTR Phase I 2010 Department of DefenseAir Force
  8. Fast, High-Order algorithms for Many-Core and GPU-based Computer Architectures

    SBC: MATHEMATICAL SYSTEMS & SOLUTIONS, INC.            Topic: AF09BT18

    We propose algorithm development and efficient GPU implementation of numerical PDE solvers based on four novel high-order methodologies: 1) High-order Discontinuous Galerkin approaches, 2) Fast High-Order boundary integral methods, 3) Convergent FFT-based methodologies for evaluation of computational boundary conditions, and 4) Fourier Continuation methods. These methodologies are applicable to a ...

    STTR Phase I 2010 Department of DefenseAir Force
  9. Coupled Cluster Methods for Multi-Reference Applications

    SBC: ACES QC, LC            Topic: AF09BT40

    The objective of Phase I is to identify the strengths and weaknesses of the various multi-reference coupled-cluster (MRCC) methods that have been proposed for the description of molecular states depending upon near degeneracies and non-dynamic electron correlation. Such effects are encountered in bond breaking, at transition states, for complex open shell systems like transition metal atoms, and f ...

    STTR Phase I 2010 Department of DefenseAir Force
  10. Theoretical Innovations in Combustion Stability Research: Integrated Analysis and Computation

    SBC: Kassoy Innovative Science Solutions            Topic: AF09BT38

    Quantitative predictions of reactive flow dynamics from large-scale simulations of Liquid Rocket Engines (LRE) appear to be model dependent. Relationships and coupling among the dominant mechanisms most responsible for destabilization are obscured by the complexities of the model and subtle consequences of inherent ad hoc approximations not supported by mathematical rationale. The reliability of ...

    STTR Phase I 2010 Department of DefenseAir Force
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