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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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.

Displaying 196161 - 196170 of 204654 results
  1. Aerodynamic Response of Out-of-Plane Wing Twist Transformation to Reduce Drag and Fuel Consumption

    SBC: ATREVIDA SCIENCE INC.            Topic: AF21ATCSO1

    The current trajectory of longer blades and taller towers for increasing wind turbine energy production is introducing additional technical, environmental, and public/social issues. Specifically, current wind turbine blade design is not optimal across all

    STTR Phase I 2021 Department of DefenseAir Force
  2. Aerodynamic Optimization for Distributed Electro Mechanical Actuators

    SBC: AURORA FLIGHT SCIENCES CORPORATION            Topic: A304

    Traditional hydraulic actuation and control surface layout both limit span wise control of lift distribution, and require large volume within wing cross-section, ultimately reducing efficiency. Mounting and support structures for traditional actuators, also necessitate drag-inducing protrusions in otherwise ideally smooth airfoils. Consequently, hydraulic systems are heavy and energy intensive as ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  3. Aerodynamic Modeling with Heterogeneous Data Assimilation and Uncertainty Quantification

    SBC: CLEAR SCIENCE CORP            Topic: A205

    Clear Science Corp. proposes to develop an aerodynamic modeling tool that assimilates data from different sources and facilitates uncertainty quantification. The technical merit and feasibility of the technology will be demonstrated in Phase I through a series of verification and validation tests that utilize both computational and wind tunnel data in constructing aerodynamic models for the Orion ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  4. Aerodynamic Microgravity Containerless Processor (AMCP)

    SBC: Orbital Technologies Corporation            Topic: N/A

    ORBITEC proposes to conduct an innovative research and development program that will result in a Aerodynamic Microgravity Containerless Processor (AMCP) technology demonstration on the International Space Station. This system will satisfy microgravity scientists that cannot currently be accommodated by the ESL, EML or acoustic systems. The innovation is based on: the use of a newly developed gas-j ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  5. Aerodynamic Materials Processing In Low-G Environments (Ample)

    SBC: Orbital Technologies Corporation            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  6. Aerodynamic Maneuvering and Control Actuation System for a Guided Destructive Expendable

    SBC: ORBITAL RESEARCH INC            Topic: N06017

    Orbital Research Inc. (ORI) is investigating the use of a rocket-powered, guided destructive expendable (GuiDE) as a next-generation countermeasure for aircraft self-protection from missile attacks. The GuiDE is aimed to provide a low-cost alternative solution to existing airborne or ground-based aircraft countermeasure systems for protecting aircraft from beamriders and shoulder-fired anti-aircra ...

    SBIR Phase II 2007 Department of DefenseNavy
  7. Aerodynamic Lift and Drag Characteristics of Irregularly Shaped Fragments

    SBC: CFD RESEARCH CORPORATION            Topic: MDA07016

    An innovative aerodynamic database generation methodology is proposed for arbitrary fragment shapes. This will be achieved with automated CFD methods, using the framework of the Unified Flow Solver (UFS). The UFS features an Adaptive Mesh and Algorithm Refinement (AMAR) procedure for seemlessly coupling rarefied and continuum algorithms inside a simulation. The AMAR automatically creates Cartesia ...

    SBIR Phase I 2008 Department of DefenseMissile Defense Agency
  8. Aerodynamic Lift and Drag Characteristics of Irregularly Shaped Fragments

    SBC: CFD RESEARCH CORPORATION            Topic: MDA07016

    An innovative aerodynamic database generation methodology is proposed for arbitrary missile fragment shapes. This will be achieved with automated CFD methods, using the framework of the Unified Flow Solver (UFS). UFS automatically creates and adapts Cartesian computational grids for arbitrary shapes and executes the analysis in an automated process, seamlessly coupling rarefied and continuum algor ...

    SBIR Phase II 2009 Department of DefenseMissile Defense Agency
  9. Aerodynamic Levitator with Active Stabilization for High-Temperature Materials Processing

    SBC: Orbital Technologies Corporation            Topic: N/A

    An innovative Earth-based aerodynamic levitator with closed-loop stability control to enhance high temperature materials processing techniques is proposed. In current approaches, turbulence-induced instability imposes limits in levitator effectiveness and limits the sample dimension capacity. With the implementation of ALAS, position instability will be reduced by closed-loop active control of sam ...

    SBIR Phase II 1995 National Aeronautics and Space Administration
  10. Aerodynamic Levitator with Active Stabilization for High-Temperature Materials Processing

    SBC: Orbital Technologies Corporation            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
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