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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. QMU in Integrated Spacecraft System Models

    SBC: ACTA, LLC            Topic: T5

    ACTA and Sandia National Laboratories propose to quantify and propagate substructure modeling uncertainty for reduced-order substructure models to higher levels of system assembly, thereby enabling predictive simulations of engineering designs with quantified margins and uncertainties for model-based flight qualification of complete spacecraft. A critical part of this process is the accurate mode ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  2. Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization

    SBC: AMERICAN GNC CORPORATION            Topic: T1

    In providing an innovative solution to improving information technologies and health management systems, AGNC is proposing a significant technological achievement with the Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization. During in-flight conditions, this system is able to not only provide the status of information such as regarding the flight envel ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  3. Process-Hardened, Multi-Analyte Sensor for Characterizing Rocket Plum Constituents Under Test Environment

    SBC: INNOSENSE CORPORATION            Topic: N/A

    The objective of the Phase II STTR project is to develop a prototype multi-analyte sensor system to detect gaseous analytes present in the test stands during propulsion test activities. Data on the concentrations of propellant-derived species are important to assure proper integration of safety protocols with testing activities to comply with environmental regulations. InnoSense LLC (ISL) has uti ...

    STTR Phase II 2009 National Aeronautics and Space Administration
  4. Health and Maintenance Status Determination and Predictive Fault Diagnosis System

    SBC: AMERICAN GNC CORPORATION            Topic: T1001

    The objective of this project is to demonstrate intelligent health and maintenance status determination and predictive fault diagnosis techniques for NASA rocket engines under online and offline conditions from either on-board or maintenance, test and analytic data. AGNC proposes a Health and Maintenance Status Determination and Predictive Fault Diagnosis System (HMSD/PFDS). The fuzzy qualitative ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  5. Benchmark Numerical Toolkits for High Performance Computing

    SBC: CFD RESEARCH CORPORATION            Topic: T501

    Computational codes in physics and engineering often use implicit solution algorithms that require linear algebra tools such as Ax=b solvers, eigenvalue, optimization, or graph algorithms. Developers face major challenges in selecting linear algebra tools that can support their algorithms, numerical schemes, meshes, and computing hardware and to minimize the time, space and complexity. The existin ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  6. High-Fidelity Gas and Granular Flow Physics Models for Rocket Exhaust Interaction with Lunar Soil

    SBC: CFD RESEARCH CORPORATION            Topic: T701

    Soil debris liberated by spacecraft landing on the lunar surface may damage and contaminate surrounding spacecraft and habitat structures. Current numerical simulations of these events lack credibility because lunar environment complexities have never been captured in suitable models: the mixed rarefied-continuum nature of the plume's surface layer flow, and the highly irregular soil particle shap ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  7. 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, performance, and controllability. The adaptable monitoring system will provide information on current and predicted aircraft performance and controllability, alerting the pilot to any aerodynamic degradation of the control effectivenes ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  8. Structural Health Monitoring with Fiber Bragg Grating and Piezo Arrays

    SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP            Topic: T201

    Intelligent Fiber Optic Systems Corporation (IFOS) in collaboration with Washington State University (WSU) proposes an approach of utilizing structurally integrated, distributed optical FBG sensor/piezo actuator arrays to monitor the health of a structure with accurate interpretation of sensor signals and real-time data processing. Our method involves a dynamic response-based damage detection tec ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  9. 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 demonstrate the feasibility of solid-state joining high strength and temperature alloys utilizing the Thermal Stir Welding process. The alloy selected for this proposed effort is Haynes 230; the alloy of choice typically utilized in rocket engine nozzel skirts. This class of alloys is difficult to fusion weld and has not been shown weldable by friction stir met ...

    STTR Phase I 2009 National Aeronautics and Space Administration
  10. Advanced Materials and Fabrication Techniques for the Orion Attitude Control Motor

    SBC: Plasma Processes, LLC            Topic: T901

    The Launch Abort System (LAS) for the Orion Crew Exploration Vehicle (CEV) will provide a safe escape for the crew in the event of an emergency during launch. A key component of the LAS is its Attitude Control Motor (ACM). Recent testing of the ACM valve assembly has resulted in failure during hot-fire testing. These failures are believed to be the result of the molybdenum alloy component disto ...

    STTR Phase I 2009 National Aeronautics and Space Administration
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