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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. High-Fidelity Gas and Granular Flow Physics Models for Rocket Exhaust Interaction with Lunar Soil

    SBC: CFD RESEARCH CORPORATION            Topic: T701

    Current modeling of Lunar and Martian soil erosion and debris transport caused by rocket plume impingement lacks essential physics from the peculiar granular characteristics of highly irregular regolith particles. Current granular mechanics models are based on mono-disperse spherical particles empiricism unsuitable for capturing the poly-disperse irregularly shaped grain mechanics. CFDRC and the U ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  2. Novel Real-Time Flight Envelope Monitoring System

    SBC: ROLLING HILLS RESEARCH CORP            Topic: T201

    The proposed innovation is an aircraft flight envelope monitoring system that will provide real-time in-cockpit estimations of aircraft flight envelope boundaries. The adaptable system will provide information on current and predicted aircraft performance and controllability, alerting the pilot to any aerodynamic degradation of the aircraft control surfaces. This includes heavy rain, in-flight i ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  3. A Reusable, Oxidizer-Cooled, Hybrid Aerospike Rocket Motor for Flight Test

    SBC: ROLLING HILLS RESEARCH CORP            Topic: T202

    The proposed innovation is to use the refrigerant capabilities of nitrous oxide (N2O) to provide the cooling required for reusable operation of an aerospike nozzle in conjunction with an N2O-HTPB (hydroxyl-terminated polybutadiene, a synthetic rubber that is used as a binder in solid rocket motors and as a fuel in hybrid rocket motors) hybrid rocket motor. The phase change cooling as liquid N2O i ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  4. Structural Health Monitoring with Fiber Bragg Grating and Piezo Arrays

    SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP            Topic: T201

    IFOS and its research institute collaborator, Washington State University (WSU), have demonstrated feasibility of a structural health monitoring (SHM) system for aerospace vehicles such as Unmanned Aerial Vehicles (UAVs) or commercial airliners. In Phase 1, a unique high-speed, high-channel count fiber Bragg grating (FBG) sensor interrogation system enabling a new Lamb wave-based damage detection ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  5. Thermal Stir Welding of High Strength and High Temperature Alloys for Aerospace Applications

    SBC: Keystone Synergistic Enterprises, LLC            Topic: T901

    The Keystone and MSU team propose to build on the successful feasibility demonstration conducted during Phase I to complete the development of solid-state joining of high strength and temperature alloys utilizing the Thermal Stir Welding process. The focus alloy for this project is Haynes 230; the alloy of choice typically utilized in rocket engine nozzel skirts. This class of alloy is difficult t ...

    STTR Phase II 2010 National Aeronautics and Space Administration
  6. Universal Superconducting Magnets for MagLifter Launch Assist Sleds

    SBC: Advanced Magnet Lab, Inc.            Topic: N/A

    NASA is considering an electromagnetic catapult, the MagLifter to lowerthe cost of cargo delivery to space. A carrier sled levitated and propelledby magnets provides the initial velocity to a space transportation vehicle.Superconducting magnets enable higher fields at lower weights than normalconducting magnets and consequently a significantly larger clearancebetween the guideway and the carrier s ...

    STTR Phase II 2001 National Aeronautics and Space Administration
  7. Automated, Parametric Geometry Modeling and Grid Generation for Turbomachinery Applications

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    The objective of this proposal is to develop a highly automated software system for rapid geometry modeling and grid generation for turbomachinery applications. The proposed system features a graphical user interface for interactive control, a direct interface to commercial CAD systems, support for IGES geometry output, and a scripting capability for parametric definition of geometries and for obt ...

    STTR Phase II 2001 National Aeronautics and Space Administration
  8. In-Situ Reductive Dehalogenation of DNAPLS By the Use of Emulsified Zero-Valent Nanoscale Iron Particles

    SBC: GeoSyntec Consultants            Topic: N/A

    This study will demonstrate the feasibility of using emulsified nanoscale iron particles to remediate pools of DNAPLs (Dense Non-Aqueous Phase Liquids) through the use of an in-situ dehalogenation process. The emulsified system will consist of a surfactant stabilized oil-in-water emulsion with the nanoscale iron particles contained within the emulsion particles. DNAPLs, such as TCE, diffuse throug ...

    STTR Phase II 2001 National Aeronautics and Space Administration
  9. Surface Functionalized Nanocarbons for Energy Storage

    SBC: Inorganic Specialists, Inc.            Topic: N/A

    Tailored carbon nanofibers are under development at Florida Atlantic University. These materials exhibit an uncommon double-layer capacitance at high frequencies; this feature makes them desirable for electrochemical capacitor applications. Their power and energy characteristics may be dramatically improved by surface functionalization using processes developed at Inorganic Specialists, Inc. Funct ...

    STTR Phase II 2001 National Aeronautics and Space Administration
  10. A Novel Liquid Hydrogen/Oxygen Co-generator

    SBC: TDA RESEARCH, INC.            Topic: N/A

    NASA¿s objective for affordable access to space requires inexpensive production of rocket fuel. The key to achieving this objective is the production of hydrogen, since hydrogen accounts for more than 80% of the fuel cost. TDA Research, Inc. (TDA), collaborating with Louisiana State University (LSU), proposes a novel hydrogen production method that offers significant advantages over conventiona ...

    STTR Phase II 2001 National Aeronautics and Space Administration
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