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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. Physics-Based Models for Aeroservoelasticity Prediction and Control

    SBC: CLEAR SCIENCE CORP            Topic: A101

    Clear Science Corp. proposes to develop and demonstrate computational fluid dynamics (CFD)-based, reduced-order aeroservoelasticity modeling and simulation technology for fast and accurate predictions of nonlinear flight dynamics, enabling real-time, piloted and unpiloted flight simulations and providing a tool to design flight controllers for highly flexible, lightweight aircraft. Physics-based, ...

    SBIR Phase II 2017 National Aeronautics and Space Administration
  2. Modeling and Controls for Synthetic Jet-Based Active Flow Control

    SBC: ACTASYS INC            Topic: A104

    In order to enable widespread application of Active Flow Control (AFC) technology on commercial transports, Actasys Inc, in collaboration with The Center for Advanced of Multifunctional Material Systems at University of California, Los Angeles (CAMMS-UCLA) and the Princeton University, intend to develop a model-based environment for the advancement of design and performance validation of AFC using ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  3. Active Flow Control (AFC) Design and System Integration Software

    SBC: CLEAR SCIENCE CORP            Topic: A104

    Clear Science Corp. proposes to develop and demonstrate computational fluid dynamics (CFD)-based software for designing and evaluating active flow control (AFC) systems on aircraft. The software will facilitate the identification of optimal types of actuation and their locations, will support virtual flight testing with both open- and closed-loop control systems, and will enable quantitative trad ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  4. Strut Attachment System for In-Space Robotic Assembly

    SBC: Honeybee Robotics, Ltd.            Topic: H504

    The size of space systems is currently limited to payload envelopes of existing launch vehicles. Due to this and the customized nature of satellites, existing space systems are very costly to stand up. Nor are they designed for repair, upgrade, or reuse to amortize the cost over multiple missions. As missions get further from low-earth orbit (LEO), the dangers of human extra-vehicular activity (EV ...

    SBIR Phase II 2017 National Aeronautics and Space Administration
  5. The Stinger: A Geotechnical Sensing Package for Robotic Scouting on a Small Planetary Rover

    SBC: Honeybee Robotics, Ltd.            Topic: H601

    The first lunar soft lander was Surveyor 1, in 1966. It had three tasks, one of which was to determine lunar surface bearing strength. Knowing the strength of the lunar surface was the single most important parameter - this essentially dictated whether landing on the Moon with significant mass like that of the Lunar Module was in fact feasible. During the Apollo program, astronauts used a Self-R ...

    SBIR Phase II 2017 National Aeronautics and Space Administration
  6. InGaAs Photomultiplier Chip Photon Counting Array for 1550 nm Operation

    SBC: Lightspin Technologies Inc            Topic: H901

    The development of a robust approach for Deep Space Optical Communications is critical to future space missions as communication bandwidth requirements are expected to dramatically increase due to continuing improvements in sensor spectral coverage and resolution. Current solutions do not meet NASAs goals for sensitivity, timing resolution, and data rate. Furthermore, many of the current solutio ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  7. SLUSH: Europa Hybrid Deep Drill

    SBC: Honeybee Robotics, Ltd.            Topic: S402

    There are at least two fundamental design approaches one could use when trying to penetrate the icy shell on Europa and other planetary bodies: a melt probe and an electro-mechanical drill. A melt probe uses a hot point to melt through ice and penetrate downward. In this regard, it is a very simple approach - it requires a heat source. However, the power required to melt 50-110K ice is 10s of k ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  8. Europa Drum Sampler (EDuS)

    SBC: Honeybee Robotics, Ltd.            Topic: S402

    The main objective of the proposed work is to develop a robust and effective sample acquisition system for the Europa lander called the Europa Drum Sampler (EDuS). The proposed drum sampling system is based on a terrestrial roadheader design and includes a Thwacker that generates percussive vibrations during rotary excavation. All components will be designed to withstand Dry Heat Microbial Red ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  9. High Temperature Stirling Cooler

    SBC: Honeybee Robotics, Ltd.            Topic: S404

    Although Honeybee and others have made huge advances in developing mechanisms, motors, and electronics for use in high temperature/high pressure environments such as the surface of Venus (460C), certain types of critical electronic and sensing technologies are inherently temperature sensitive. The lack of high temperature tolerat cameras and optical sensors has, to date, prevented up-close in-sit ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  10. High Effectiveness and Low Pressure Drop Recuperator for Closed Brayton Cycle Turboalternator

    SBC: MOHAWK INNOVATIVE TECHNOLOGY, INC.            Topic: Z103

    Under this Phase I effort, MiTi proposes to establish the design of a high performance recuperator for integration with a Close Brayton Cycle turboalternator for space application, primarily for fission-based power generation technologies for surface missions on the moon and Mars. The proposed recuperator design will emphasize high effectiveness approaching or exceeding 90% in addition to being s ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
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