You are here

Award Data

For best search results, use the search terms first and then apply the filters
Reset

The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

  1. Antistatic Thermal Control Coatings

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Electrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  2. Antistatic Thermal Control Coatings

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Electrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  3. Self-Deploying Foam Antenna Structures

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Inflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...

    STTR Phase I 2002 National Aeronautics and Space Administration
  4. Self-Deploying Foam Antenna Structures

    SBC: Adherent Technologies, Inc.            Topic: N/A

    Inflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...

    STTR Phase II 2002 National Aeronautics and Space Administration
  5. Spacesuit Monitor

    SBC: Adherent Technologies, Inc.            Topic: N/A

    The concentration of carbon dioxide in exhaled breath is 3.8%; a concentration of 2% causes deepened breathing, and 4% causes a marked increase in respiration. These higher concentrations of CO2 also cause drowsiness and can be unsafe. Therefore, it is desirable to monitor the concentration of CO2 in exhaled breath to guarantee the safety of an astronaut in the dangerous extravehicular environment ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  6. Low Cost Engine Test Stand for 500 lb Thrust Class Engines

    SBC: AJT and Associates, Inc            Topic: N/A

    AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard test-stand interface, greatly reducing the time required to install and remove various engines. Thi ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  7. Low Cost Engine Test Stand for 500 lb Thrust Class Engines

    SBC: AJT and Associates, Inc            Topic: N/A

    AJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard test-stand interface, greatly reducing the time required to install and remove various engines. Thi ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  8. Magnetohydrodynamic Stable Reference (MSTAR)

    SBC: A-TECH CORPORATION            Topic: N/A

    Platforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  9. Magnetohydrodynamic Stable Reference (MSTAR)

    SBC: A-TECH CORPORATION            Topic: N/A

    Platforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  10. Nano Ceramic Sterilization Filter

    SBC: ARGONIDE CORP.            Topic: N/A

    Filters don't exist that are capable of removing virus and bacteria at high enough flow rates to be practical either for space systems or for domestic consumption. In Phase 1 we demonstrated feasibility that our nano ceramic fiber filter could produce sterile water at high flow rates. In Phase 2 we propose to develop performance data on such filters that would provide NASA with the capability for ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
US Flag An Official Website of the United States Government