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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. THE PRIMARY PURPOSE OF THIS PROJECT IS TO REDUCE THE REQUIREMENTS FOR INITIAL ALIGNMENT ACCURACY WHEN BRINGING A PAIR OF CONNECTORS TOGETHER PRIOR TO MATING THEM.

    SBC: Arbus, Inc.            Topic: N/A

    THE PRIMARY PURPOSE OF THIS PROJECT IS TO REDUCE THE REQUIREMENTS FOR INITIAL ALIGNMENT ACCURACY WHEN BRINGING A PAIR OF CONNECTORS TOGETHER PRIOR TO MATING THEM. THIS WILL BE ACCOMPLISHED BY INVESTIGATING THE USE OF A TAPERED OR CONICAL DESIGN TO INCLUDE A PRELIMINARY LATCHING FEATURE TO CAPTURE AND TO CAUSE ALIGNMENT OF A PAIR OF COMPLEMENTARY CONNECTORS. THE INVESTIGATION WILL TAKE INTO CONSIDE ...

    SBIR Phase I 1984 National Aeronautics and Space Administration
  2. N/A

    SBC: GSE, Inc.            Topic: N/A

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  3. Affordable High Power Density Engine Designs for Personal Air Vehicles

    SBC: GSE, Inc.            Topic: N/A

    Next generation General Aviation (GA) Sport Class air vehicles limited to 1200lbs, represent the first opportunity to overhaul the FAA certification process necessary to manufacture affordable aircraft. With propulsion representing over one-third of the direct manufacturing costs of the entire aircraft, dramatic reductions in aircraft engine costs must be achieved by design, economy of scale, and ...

    STTR Phase II 2005 National Aeronautics and Space Administration
  4. Affordable High Power Density Engine Designs for Personal Air Vehicles

    SBC: GSE, Inc.            Topic: T701

    Next generation General Aviation (GA) Sport Class air vehicles limited to 1200lbs, represent the first opportunity to overhaul the FAA certification process necessary to manufacture affordable aircraft. With propulsion representing over one-third of the direct manufacturing costs of the entire aircraft, dramatic reductions in aircraft engine costs must be achieved by design, economy of scale, and ...

    STTR Phase I 2004 National Aeronautics and Space Administration
  5. An Integrated Heavy Fuel Piston Engine Ducted Fan Propulsion Unit for Personal Air Vehicles

    SBC: GSE, Inc.            Topic: T701

    The proposed PAVE propulsion system technology demonstration combines an innovative high-speed aero-diesel engine with a novel ducted fan assembly resulting in a low noise/cost and high performance propulsion system. The core engine makes extensive use of a novel self-injection, compression ignition/combustion system capable of high-speed operation on kerosene-based fuels without degradation due ...

    STTR Phase I 2004 National Aeronautics and Space Administration
  6. An Integrated Heavy Fuel Piston Engine Ducted Fan Propulsion Unit for Personal Air Vehicles

    SBC: GSE, Inc.            Topic: N/A

    The proposed PAVE propulsion system technology demonstration combines an innovative high-speed aero-diesel engine with a novel ducted fan assembly resulting in a low noise/cost and high performance propulsion system. The core engine makes extensive use of a novel self-injection, compression ignition/combustion system capable of high-speed operation on kerosene-based fuels without degradation due t ...

    STTR Phase II 2005 National Aeronautics and Space Administration
  7. 200 Hp Ga Diesel Propulsion System

    SBC: GSE, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  8. Natural Tracking Control For Telerobotic Servicing Robots

    SBC: M&m Technologies Inc.            Topic: N/A

    N/A

    SBIR Phase I 1995 National Aeronautics and Space Administration
  9. GENERAL PURPOSE, OPTICAL, VECTOR-MATRIX MULTIPLIER

    SBC: OPTICOMP CORP.            Topic: N/A

    A GENERAL PURPOSE, OPTICAL, VECTOR-MATRIX MULTIPLIER WILL BE DEVISED TO COMPUTE 256X256 ELEMENT MATRICES TIMES 256-ELEMENT VECTORS AT 8-BITS PRECISION IN LESS THAN 100 MICROSECONDS. THIS PROJECT WILL TAKE AN INNOVATIVE ARCHITECTURAL APPROACH THAT USES TWO 64-CHANNEL ACOUSTO-OPTIC DEVICES OPERATING AT SEVERAL HUNDRED MEGAHERTZPER CHANNEL IN A TELECENTRICALLY IMAGED CONFIGURATION. THE USE OF LASER D ...

    SBIR Phase I 1991 National Aeronautics and Space Administration
  10. HIGH DENSITY CHEMICAL THERMAL STORAGE SYSTEM FOR LOW GRAVITY ENVIRONMENTS

    SBC: Rocky Research            Topic: N/A

    THERMAL STORAGE SYSTEMS ARE NEEDED FOR EFFECTIVE THERMAL MANAGEMENT ON MANNED SPACECRAFT AND PLANETARY BASED SYSTEMS. THERMAL STORAGE EQUIPMENT HAS THE POTENTIAL TO REDUCE THE OVERALL SYSTEM MASS BY DECREASING THE CAPACITY REQUIREMENTS OF HEAT PUMPS, REFRIGERATORS AND CHILLERS THROUGH LOAD LEVELING. TODAY'S THERMAL STORAGE CONCEPTS, HOWEVER, ARE INADEQUATE FOR SPACE APPLICATION, SINCE THE ENERGY D ...

    SBIR Phase II 1991 National Aeronautics and Space Administration

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