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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. Intelligent Control For Autonomous Remote Spacecraft

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    We will apply the latest knowledge in learning control, adaptive control, and optimal control to develop a modular, state-of-the-art, adaptive, nonlinear, guidance, navigation, and control package for remote spacecraft. The system will incorporate planning and decision making modules to give the remote spacecraft on-line goal directed self-reliant behavior with a high degree of autonomy. At the hi ...

    STTR Phase I 2001 National Aeronautics and Space Administration
  2. MagLev Launch Propulsion for LoFLYTE¿Waverider Unmanned Aerial Vehicle

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation, teamed with PRT Advanced Maglev Systems, will work together to perform flight test experiments for launching the LoFLYTE¿ UAV from NASA Marshall Space Flight Center¿s 100-foot outdoor Maglev track. The goal of the Phase I program is to lay the foundation for a Phase II flight test program that will demonstrate the use of the Maglev track to launch a hypersonic configuration ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  3. Friction Drag Reduction System

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation Corporation proposes to design a system for reducing the friction drag on an aircraft by introducing an ion space charge into the aircraft¿s boundary layer. We will develop a detailed model for the drag reduction mechanism; evaluate the system performance; evaluate alternative electromagnetic and/ or mechanical processes for generating a space charge in the boundary layer of a ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  4. Friction Drag Reduction System

    SBC: ACCURATE AUTOMATION CORPORATION            Topic: N/A

    Accurate Automation Corporation proposes to design a system for reducing the friction drag on an aircraft by introducing an ion space charge into the aircraft¿s boundary layer. We will develop a detailed model for the drag reduction mechanism; evaluate the system performance; evaluate alternative electromagnetic and/ or mechanical processes for generating a space charge in the boundary layer of a ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  5. A General Computer Code for Simulation of Plasma Aerodynamics and Propulsion

    SBC: LYTEC LLC            Topic: N/A

    Lytec LLC proposes to integrate the simulation technology of the MagnetoHydroDynamic (MHD) community into the worlds leading propulsion and aerodynamic flow solver WIND. The WIND code has been chosen because of its general acceptance in the aerospace community as a first class flow simulation tool. The ultimate goal is to provide an integrated magnetogasdynamic solver that will advance the state o ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  6. Robotic Bioreactor for Cell Culture in Space Applications (DYNACULT)

    SBC: TECHSHOT, INC.            Topic: N/A

    The specific innovation proposed is a fully-automated perfused cell-culture bioreactor system (laboratory in a cassette) tentatively named DYNACULT. Space Hardware Optimization Technology, Inc.,will incorporate several technical innovations into the integrated DYNACULT system. These include, but are not limited to, options for gentle mixing of cell and/or microcarrier suspensions independently var ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  7. Observation Chambers for Dynamic Microscopic Flow Visualization (DYNASCOPE)

    SBC: TECHSHOT, INC.            Topic: N/A

    The specific innovation proposed, tentatively named ¿DYNASCOPE¿, is an innovative system of microscopy equipment capable of unique sample manipulation and real-time observation. A uniquely designed hollow microscope slide with high manufacturability offers an opportunity to study the effects of capillary forces, magnetic fields, electrokinetic fields, and microscopic hydrodynamics on a wide ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  8. Reliability Prediction Model for Large, Reusable Propellant Tanks

    SBC: VEXTEC CORPORATION            Topic: N/A

    NASA has defined goals for development of future reusable launch vehicles (RLV). Systems must be reliable with less than 1 flight failure in 10,000 missions with mission cost of 1000 dollars per pound per payload (or less). X-33 propellant tank incidents indicate need for improving state-of-the-art design and/or manufacture of composite storage tanks. Bond integrity has been an issue during develo ...

    SBIR Phase I 2001 National Aeronautics and Space Administration

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