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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. 200 Hp Ga Diesel Propulsion System

    SBC: GSE, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  2. A Green, Safe, Dual-Pulse Solid Motor for CubeSat Orbit Changing

    SBC: Digital Solid State Propulsion, Inc            Topic: S302

    Small satellites such as CubeSats are in need of responsive propulsion, but are limited due to their size. Though single pulse, AP/HTPB fueled solid rocket motors exist in the market, greater mission flexibility is to be had from a motor with the capability of a second ignition in the same volume constraints. Digital Solid State Propulsion (DSSP) proposes research into the technology to not only t ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  3. A Green, Safe, Multi-Pulse Solid Motor (MPM) for CubeSats

    SBC: Digital Solid State Propulsion, Inc            Topic: S302

    Today's CubeSats lack storable, green, safe propulsion options for complex science missions that may involve large Delta-V changes, proximity operations, and attitude control systems (ACS) for pointing, spin-up, and spin-down. Digital Solid State Propulsion (DSSP) is developing propulsion for CubeSats and will leverage existing research efforts into a new system for NASA. A key technology identifi ...

    SBIR Phase II 2015 National Aeronautics and Space Administration
  4. 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
  5. 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
  6. AIRBORNE WEATHER RADAR FOR WINDSHEAR WARNING

    SBC: Sierra Nevada Corporation            Topic: N/A

    NUMEROUS AIRCRAFT ACCIDENTS HAVE OCCURED DURING TAKEOFF AND LANDING DUE TO THE STRONG AND UNEXPECTED WINDS DIVERGING FROM A MICROBURST OUTFLOW. EXTENSIVE RESEARCH HAS INDICATEDTHAT IT IS POSSIBLE TO DETECT SUCH WINDS BY MEANS OF A DOPPLER WEATHER RADAR. A LOGICAL RADAR CANDIDATE IS THE UNIT CARRIED BY ALL AIR TRANSPORTS. A PROBLEM WITH THE USE OF SUCH INSTALLED RADARS IS THEIR LOWPRF (PULSE REPETI ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  7. An Innovative Method of NOX Reduction Through Fuel Additives for the UEET Program

    SBC: Software And Engineering Associates, Inc.            Topic: N/A

    The opportunity addressed in this proposal is to transfer a fuel-additive technology developed for NOx and particulate matter reduction in diesel fuels, to applications in ultra-efficient jet engine fuels, with no reduction in performance and power output of the engine. The innovation is based on a novel fuel additive, PuriNOx(TM), developed by Lubrizol Corporation. Unlike conventional fuel additi ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  8. 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
  9. 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
  10. Fabrication of T-SOFC via Freeze Cast Methods for Space and Portable Applications

    SBC: Yanhai Power LLC            Topic: H801

    As NASA space missions become longer in duration the need for high efficiency power generator sets that can operate on NASA logistical fuel become critical. Historically NASA has used fuel cells as part of the energy solution. Space bound energy and power systems require rapid start and stop cycle times as well as high power densities. The high operational efficiency, coupled with the use of logi ...

    SBIR Phase I 2014 National Aeronautics and Space Administration

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