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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. Air Vehicle Optimization for Efficient and Precision Payload Delivery and Reconnaissance

    SBC: Prioria Robotics, Inc.            Topic: SOCOM172004

    Prioria is proposing a family of aircraft configurations to address USSOCOM's requirements. Achieving the significant endurance, range, winds, and payload requirements simultaneously requires a highly-optimized aircraft. The configurations range in endurance, robustness, and capability. Configuration 1 is a sturdy fixed-wing aircraft that achieves moderate endurance but can tolerate rough handl ...

    SBIR Phase I 2017 Department of DefenseSpecial Operations Command
  2. Feasibility and design study for the development of a low acoustic emission UAV propulsion unit.

    SBC: Cobb Design Inc            Topic: SOCOM163001

    The proposed study will evaluate the feasibility of producing a low acoustic emission propulsion unit for fixed wing UAV applications, utilizing optimized propeller designs matched to a low cylinder count small reciprocating engine. Acoustic performance will be enhanced by operating the propeller at reduced speed with high advance while improving the operating point of the coupled engine and furt ...

    SBIR Phase I 2017 Department of DefenseSpecial Operations Command
  3. High Performance Simulation Tool for Multiphysics Propulsion Using Fidelity-Adaptive Combustion Modeling

    SBC: STREAMLINE NUMERICS, INC.            Topic: T102

    The innovation proposed here is a fidelity-adaptive combustion model (FAM) implemented into the Loci-STREAM CFD code for use at NASA for simulation of rocket combustion. This work will result in a high-fidelity, high-performance multiphysics simulation capability to enhance NASA's current simulation capability of unsteady turbulent reacting flows involving cryogenic propellants. This novel FAM m ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  4. Vision-Based Navigation for Formation Flight onboard ISS

    SBC: JAYCON SYSTEMS LLC            Topic: T1102

    The RINGS project (Resonant Inductive Near-field Generation Systems) was a DARPA-funded effort to demonstrate Electromagnetic Formation Flight and wireless power transfer in microgravity. Integration inconsistencies in both hardware and software prevented the experiment from achieving its objectives during the planned test sessions. A later project supported by NASA ARC focused on the assessment, ...

    STTR Phase I 2017 National Aeronautics and Space Administration
  5. Fast Response, Fiber-Optic Micromachined Five-Hole Probe for Three-Dimensional Flow Measurements in Harsh Environments

    SBC: INTERDISCIPLINARY CONSULTING CORP            Topic: A108

    The Interdisciplinary Consulting Corporation (IC2) proposes the development of a fiber-optic, micromachined five-hole probe for three-dimensional flow measurements in harsh environments. The goal of this research is to develop a microelectromechanical systems (MEMS) based, optical probe capable of significantly improved performance compared to existing available sensors, by enabling faster respons ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  6. High Channel Count, High Density Microphone Arrays for Wind Tunnel Environments

    SBC: INTERDISCIPLINARY CONSULTING CORP            Topic: A102

    The Interdisciplinary Consulting Corporation (IC2) proposes the development of high channel count, high density, reduced cost per channel, directional microphone arrays for noise source measurement using microelectromechanical systems (MEMS) based piezoelectric microphones with backside contacts and advanced packaging technology. The goal of this research is to develop an advanced phased-array te ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  7. High Lift Heat Pump

    SBC: MAINSTREAM ENGINEERING CORP            Topic: Z201

    NASA has identified a need for higher heat rejection temperatures due to an equatorial lunar mission profile, where surface temperatures reach 400 K. To meet this need for space exploration vehicles to reject waste heat to high temperature heat sinks, Mainstream proposes adapting our oil-less vapor-compression (V-C) refrigeration compressor technology for operation at high temperature and high li ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  8. Intelligent Electronic Speed Controller

    SBC: 4D TECH SOLUTIONS, LLC            Topic: A106

    This project intends to design and develop an Intelligent Electronic Speed Controller (IESC) for use on Unmanned Aerial Vehicles (UAVs). The IESC will advance the state-of-the-art of health-state awareness. This will be achieved through the integration of propulsion system health monitoring sensors that - in unison with an Intelligent Rule Set - will be able to monitor system and component perfo ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  9. Ultra-Lightweight Multifunctional Magnesium Alloy Shielding Structures

    SBC: INNOVATIVE SPACE TECHNOLOGIES LLC            Topic: H1101

    Radiation from GCRs and Solar Flares provide a hostile ionizing environment for personnel and vital electronic systems. The effects of this environment has been a topic of research for many years. Issues include the exposure for humans under acute and continuous exposures and the radiogenic cancer risk that rises with total dose and is a limiting constraint on long-duration missions. The propose ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  10. Affordable Integrated GPS-Actuator GN&C System for Small Launch Vehicles

    SBC: MICRO AEROSPACE SOLUTIONS INC            Topic: Z901

    A small launcher GNC system which maintains GPS fix while rotating, improves drift performance for COTS-based inertial sensors and provides efficient use of actuation system propellant. Provided in a package with components and systems already under development and proven in the space environment. Phase I will result in a flight test ready system

    SBIR Phase I 2017 National Aeronautics and Space Administration
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