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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. An Affordable Autonomous Hydrogen Flame Detection System for Rocket Propulsion

    SBC: INNOVATIVE IMAGING & RESEARCH CORP            Topic: H1001

    NASA has long used liquid hydrogen as a fuel and plans to continue using it in association with their advanced nuclear thermal propulsion technology. Hydrogen fire detection is critical for rocket propulsion safety and maintenance. A significant fire at a rocket test or launch facility could be catastrophic to infrastructure or even worse, to human life. Detection monitoring is problematic as hydr ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  2. Color-XHDR- A Compact High-Speed Color Extreme High Dynamic Range Video Capability for Rocket Engine Testing

    SBC: INNOVATIVE IMAGING & RESEARCH CORP            Topic: H1002

    Innovative Imaging and Research proposes to develop a 21st Century color, high-speed extreme high dynamic range (Color-XHDR) video recording technology that will produce engineering-grade video to accurately document rocket motor firings at close range within a test cell without image saturation. This novel imaging system will include a compact, single focal plane array camera and end-to-end image ...

    SBIR Phase II 2017 National Aeronautics and Space Administration
  3. Synthesis of HAN and HEHN in a Continuous Mix Process

    SBC: Digital Solid State Propulsion, Inc            Topic: AF171061

    Production of hydroxylamine nitrate (HAN) and hydroxyethyl hydrazine nitrate (HEHN) is of great concern for the manufacture of AF-315E. Current stockpiles of heritage ingredients held by AFRL are being depleted and those manufacturers are no longer in exi

    SBIR Phase I 2017 Department of DefenseAir Force
  4. High Voltage (HV) Fireset Systems and Subsystem Component Level Designs

    SBC: HYPERION TECHNOLOGY GROUP INC            Topic: AF171089

    Current and future explosive munition weapon systems development relies heavily on explosives detonation performance characterization and computational hydro-code simulation research conducted by DoD and DoE research communities. This work in turn relies

    SBIR Phase I 2017 Department of DefenseAir Force
  5. Prediction and Measurement of the Soot Build-Up in Film-Cooled Rocket Engines

    SBC: SIERRA ENGINEERING, INC.            Topic: AF15AT21

    This Phase II STTR effort is focused on generating the data necessary to identify the phenomenology that produces carbon deposition within kerosene film cooled rocket engines.This data is essential to guide the model development and validation process.Program outputs will be both data and a physics-based model for carbon deposition.

    STTR Phase II 2017 Department of DefenseAir Force
  6. Energy Efficient LED Spectrally Matched Smart Lighting

    SBC: INNOVATIVE IMAGING & RESEARCH CORP            Topic: T1002

    Innovative Imaging and Research and the University of Houston Clear Lake have teamed to develop a widely extensible, affordable, energy efficient, smart lighting device known as Lambda-Net. Smart building technologies, such as Lambda-Net, are becoming critical to energy savings and sustainability for terrestrial applications and space-based habitats. Our device incorporates a smart-mobile device ...

    STTR Phase II 2013 National Aeronautics and Space Administration
  7. Computational Modeling of Coupled Acoustic and Combustion Phenomena Inherent to Gas Turbine Engines

    SBC: Flow Modeling and Simulation            Topic: AF131181

    ABSTRACT: Flow Modeling and Simulation, LLC (FMS), proposes to develop a computational software tool, herein designated AUG3D, that is intended to provide physics-based, multi-level, validated computational simulations of turbine engine component flow fields, particularly those associated with thrust augmentors, i.e., afterburners. This tool will be ideally suited for closely integrating physica ...

    SBIR Phase I 2013 Department of DefenseAir Force
  8. Advanced Analysis and Design Tool for Scramjet Air-frame Propulsion Integration

    SBC: Flow Modeling and Simulation            Topic: AF112004

    ABSTRACT: The SCRAMSIM computer code will be able to perform analysis for engineering design, stemming from a low order Reynolds Average Navier-Stokes (RANS) to high order (4th or higher) LES using accurate subgrid scale models (SGS). It will also solve thermal non-equilibrium mechanisms, conjugated heat transfer, general finite-rate chemistry using several databases for hydrocarbon/hydrogen-air ...

    SBIR Phase II 2013 Department of DefenseAir Force
  9. Method of Locating Unexploded Ordnance

    SBC: MAV6            Topic: AF083236

    The Unexploded Ordnance Asset RFID System (UARS) is an active low frequency RFID tracking system designed for locating unexploded ordinance (UXO) on the battlefield.  The system is a passive thin collar RFID tag that is placed onto the munition during manufacture and becomes activated after delivery on target.  Once activated, the RFID tag enters a passive listening mode, waiting for a specific ...

    SBIR Phase I 2009 Department of DefenseAir Force
  10. Scramjet Combustion Stability Behavior Modeling

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: N/A

    A recent breakthrough in combustion stability analysis (UCDS) offers the means to accurately predict the combustion stability of a scramjet. This capability is very important due to the extreme scramjet operational environment, which makes cut-and-try development approaches impractical. With UCDS, it is now possible to accurately predict the scramjet pressure oscillation amplitudes, along with c ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
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