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The Award database is continually updated throughout the year. As a result, data for the given year is not complete until April of the following year. Annual Reports data is a snapshot of agency reported information for that year and hence might look different from the live data in the Awards Information charts.

  1. Optical Line Filter and Spectrometer based Upon Two-Photon Absorption for Doppler LIDAR at 1.053 um

    SBC: ESPYLUX LLC            Topic: S1

    A receiver system for use in LIDAR consisting of an optical filter and optical spectrometer based upon two-photon absorption is proposed.  The filter and spectrometer both use dispersion from excited state transitions of atomic rubidium  to create a birefringent medium. The birefringent medium of the optical filter rotates the polarization of light so that it is transmitted through cross ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  2. Fail-Safe, Controllable Liquid Spring/Damper System for Improved Rover Space Vehicle Mobility

    SBC: Advanced Materials and Devices            Topic: H601

    NASA is planning to return to the moon in 2020 to explore thousands of miles of the moon?s surface with individual missions, lasting six months or longer. Surface mobility is critical to outpost buildup and exploration activities, where the change in the vehicle weight between unloaded and loaded cargo conditions and travel over rough terrain can adversely affect the ride handling conditions and ...

    SBIR Phase I 2016 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. Green Electric Monopropellant (GEM) Fueled Pulsed Plasma Thruster

    SBC: Digital Solid State Propulsion, Inc            Topic: S302

    Digital Solid State Propulsion is proposing the development of a new liquid Pulsed Plasma Thruster (PPT) using its revolutionary HAN-based Green Electric Monopropellant (GEM) to enable spacecraft missions whose fulfillment requires the high specific impulse of conventional Telfon-fueled PPTs, but would like the flexibility in mission design that liquid fueled systems allow. DSSP's GEM propellant i ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  5. 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
  6. Plume Diagnostics for Combustion Stability

    SBC: SIERRA ENGINEERING, INC.            Topic: T901

    Sierra Engineering Inc. and Purdue University propose to develop a non-intrusive plume instrument capable of detecting and diagnosing combustion instability. This Stability Diagnostic System (SDS) will be designed, assembled, and tested during this effort. The SDS will include a high-speed video camera and multiple photodiode detectors for observing the plume. It will also include a software pa ...

    STTR Phase II 2007 National Aeronautics and Space Administration
  7. Triaxial Swirler Liquid Injector Development

    SBC: SIERRA ENGINEERING, INC.            Topic: X601

    Sierra Engineering Inc. (Sierra) believes that the subject triaxial liquid propellant swirl injector has the potential to meet many of NASA's Earth-to-Orbit (ETO) propulsion systems goals. The triaxial swirl injector is ideally suited to a wide range of liquid oxidizers and fuels, including hydrogen and a wide range of hydrocarbons. It holds the potential of excellent high-frequency combustion st ...

    SBIR Phase II 2006 National Aeronautics and Space Administration
  8. Plume Diagnostics for Combustion Stability

    SBC: SIERRA ENGINEERING, INC.            Topic: T901

    Sierra Engineering and Purdue University propose to leverage combustion stability testing, already funded and planned for the second and third quarters of next year at Purdue, by developing a non-intrusive plume instrument capable of detecting combustion instability and testing it during combustor firings. Purdue has previously created the combustor and demonstrated unstable combustion operation. ...

    STTR Phase I 2006 National Aeronautics and Space Administration
  9. Hybrid Prediction Method for Aircraft Interior Noise

    SBC: ESI US R&D            Topic: A204

    The goal of the project is research and development of methods for application of the Hybrid FE-SEA method to aircraft vibro-acoustic problems. This proposal discusses the development and application of new methods of structural-acoustic analysis in order to address existing problems in aircraft interior noise prediction. The proposed methods are based on a hybrid modeling strategy that combines ...

    SBIR Phase II 2006 National Aeronautics and Space Administration
  10. 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

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