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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. 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. 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
  4. 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 II 2015 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. 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
  8. FIR Detectors/Cameras Based on GaN and Si Field-Effect Devices

    SBC: Sensor Electronic Technology, Inc.            Topic: S104

    SETI proposes to develop GaN and Si based multicolor FIR/THz cameras with detector elements and readout, signal processing electronics integrated on a single chip. The active detector elements will be submicron gated channels with 2 dimensional electron gas (2DEG). The devices with gated 2DEG (commonly known as field-effect transistors) respond to the incoming FIR radiation due to the rectificat ...

    SBIR Phase I 2009 National Aeronautics and Space Administration
  9. 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
  10. 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

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