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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. HIGH LIFT HEAT ACTUATED SOLID-VAPOR HEAT PUMP FOR SIMULTANEOUS REFRIGERATION AND WATER HEATING.

    SBC: Rocky Research            Topic: N/A

    THERE IS A NEED FOR REFRIGERATION AS WELL AS HOT WATER HEATING ON MANNED SPACECRAFT. IN ORDER TO OBTAIN ENERGY ANDMASS EFFICIENT EQUIPMENT, IT IS PROPOSED TO USE COORDINATIVECOMPLEX COMPOUNDS, A SPECIAL CLASS OF NON-TOXIC SOLID-VAPOR MEDIA, FOR A DUAL DUTY THERMODYNAMIC CYCLE WHICH PROVIDES SIMULTANEOUSLY REFRIGERATION AND HOT WATER HEATING. SUCH CYCLES CAN BE DRIVEN WITH RELATIVELY LOW TEMPERATUR ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  3. HIGH DENSITY CHEMICAL THERMAL STORAGE SYSTEM FOR LOW GRAVITY ENVIRONMENTS

    SBC: Rocky Research            Topic: N/A

    N/A

    SBIR Phase I 1990 National Aeronautics and Space Administration
  4. THE CHEMICAL KINETICS OF LOX/HYDROCARBON COMBUSTION

    SBC: Software & Engineering Associa            Topic: N/A

    ANALYTICAL METHODS AND COMPUTER SOFTWARE ARE TO BE DEVELOPED FOR CHARACTERIZING THE CHEMICAL KINETIC MECHANISMS THAT CONTROL LOX/HYDROCARBON COMBUSTION IN ROCKET ENGINES. CRITICAL AREAS OF TECHNOLOGY ARE TO BE IDENTIFIED. AN INNOVATIVE AND HIGHLY GENERAL METHOD WILL BEAPPLIED TO MODEL LOX/RP-1 COMBUSTION AS IT OCCURS IN GAS GENERATORS FOR PUMP FED ENGINES. THE METHOD WILL THEN BE EXTENDED TO MODEL ...

    SBIR Phase II 1990 National Aeronautics and Space Administration

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