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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. Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center

    SBC: ACCUDYNE SYSTEMS, INC.            Topic: A404

    Reduced mass composite materials are crucial to the success of aerospace systems, but are inhibited by expensive autoclave consolidation, especially for large parts. To remedy this, NASA-LaRC has been developing cost-effective high-performance thermoplastic composite materials for years. NASA materials could dramatically reduce the cost of large aerospace structures, because those materials avo ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  2. Advanced Actuator Concepts for High Precision Deformable Mirrors

    SBC: TRS CERAMICS, INC.            Topic: S303

    TRS Technologies proposes to develop a variety of single crystal actuators for adaptive optics deformable mirrors. Single crystal piezoelectric actuators are proposed as a means of increasing actuator authority while maintaining strain precision for adaptive optics deformable mirrors used in future space observatory missions. Single crystals based on PZN-PT or PMN-PT represent a revolutionary ad ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  3. Single Crystal Piezomotor for Large Stroke, High Precision and Cryogenic Actuations

    SBC: TRS CERAMICS, INC.            Topic: S205

    TRS Technologies proposes a novel single crystal piezomotor for large stroke, high precision, and cryogenic actuations with capability of position set-hold with power-off. The proposed concept will advance the state-of-art cryogenic actuations considering the excellent cryogenic properties (with d33 and d31 at 30K similar or higher than that of PZT at room temperature) and the great electromechan ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  4. High Temperature Electrostrictive Ceramics

    SBC: TRS CERAMICS, INC.            Topic: S402

    TRS Technologies proposes to develop high temperature electrostrictors from bismuth-based ferroelectrics. These materials will exhibit high strain and low loss in the 400 to 500?C temperature range, enabling the development of robotic components such as high power ultrasonic transducers and high force actuators for NASA?s planned missions to Venus. Such devices are currently made from piezoelect ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  5. Cryogenic Capacitors for Low-Temperature Power Systems

    SBC: TRS CERAMICS, INC.            Topic: S404

    TRS Technologies proposes to develop low-temperature multilayer ceramic capacitors (MLCCs) capable of operating at cyrogenic temperatures (

    SBIR Phase I 2004 National Aeronautics and Space Administration
  6. Modeling Unsteady Cavitation Effects and Dynamic Loads in Cryogenic Systems

    SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC            Topic: A406

    There currently are no analytical or CFD tools that can reliably predict unsteady cavitation dynamics in liquid rocket cryogenic systems. Analysis of cavitating cryogenic systems presents a challenge, and is poorly understood, because the phase change process couples with the temperature fluctuations in the fluid. In particular when large scale flow unsteadiness is present at low-flow, off-desig ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  7. Smart Materials Technology for High Speed Adaptive Inlet/Nozzle Design

    SBC: CONTINUUM DYNAMICS INC            Topic: A203

    Enabling a new generation of high speed civil aircraft will require breakthrough developments in propulsion design, including novel techniques to optimize inlet performance across a wide speed range. Maximizing propulsive performance while minimizing weight and mechanical complexity is a key goal for such systems, and rapidly maturing smart materials technology can enable adaptive control of inle ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  8. System Compliant Actuation for Structural Engine Noise Remission

    SBC: QORTEK INC            Topic: A204

    The purpose of the research into ?Compliant Actuator? design will be to demonstrate to prototype level a low profile fully integrated control mechanism. This mechanism will be the first of its kind in that it enables independent multifunctionally integrated control including all i/o, processing, control and power functions in a single compliant package that uses a active piezoceramic substrate. A ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  9. Low Permeation Envelope Material Development for Titan Aerobot

    SBC: Lamart Corporation            Topic: S202

    Aerobot vehicles for missions on Titan require envelope materials that are strong, light and durable. Unlike terrestrial balloon materials, these must be able to withstand flexing at temperatures of 90K without developing pinhole leaks. To meet this requirement, it is proposed to use Lamart?s experience in lightweight laminated sailcloth and ultra light film lamination to create a material for thi ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  10. Investigation of Non Eroding Nozzle Materials for Optimized Coated Hybrid Leading Edge Designs For Reusable Launch Vehicals With Leading Edge Radii of 0.03? TO 1? and Temperatures Near 4000?F

    SBC: MATERIALS RESEARCH & DESIGN INC            Topic: A404

    Effort explores using innovative hybrid reinforced carbon-carbon, refractory ceramics, super alloys and composite materials as thermal protection system specifically in the 4000?F range with leading edge radii of between 0.03? and 1.0?. The RLV leading edge is the primary TPS that space vehicles use re-entering the atmosphere traveling at hypersonic speeds. Depending on the Mach number spacecraft ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
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