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  1. 1
    Second Magnetoplasmadynamic Thruster Workshop : proceedings of a workshop sponsored by and held at NASA Lewis Research Center, May 19, 1992.
    Published 1992
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    Government Document Conference Proceeding Microform Book
  2. 2
    Spatially-resolved beam current and charge-state distributions for the NEXT ion engine /
    Published 2010
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    Government Document Conference Proceeding eBook
  3. 3
    An optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation /
    by Litt, Jonathan S.
    Published 2005
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    Government Document Conference Proceeding eBook
  4. 4
    Thrust stand characterization of the NASA Evolutionary Xenon Thruster (NEXT) /
    Published 2010
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    Government Document Conference Proceeding eBook
  5. 5
    An optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation /
    by Litt, Jonathan S.
    Published 2005
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    connect to online version. (PDF)
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    Government Document Conference Proceeding eBook
  6. 6
    Spatially-resolved beam current and charge-state distributions for the NEXT ion engine /
    Published 2010
    Get full text
    connect to online version. (PDF)
    Get full text
    Government Document Conference Proceeding eBook
  7. 7
    Thrust stand characterization of the NASA Evolutionary Xenon Thruster (NEXT) /
    Published 2010
    Get full text
    connect to online version. (PDF)
    Get full text
    Government Document Conference Proceeding eBook
  8. 8
    Modeling neutral densities downstream of a gridded ion thruster /
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    Government Document Conference Proceeding eBook
  9. 9
    NASA's Evolutionary Xenon Thruster (NEXT) Prototype Model 1R (PM1R) ion thruster and propellant management system wear test results /
    by Van Noord, Jonathan L.
    Published 2010
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    Government Document Conference Proceeding eBook
  10. 10
    Application of the NEXT ion thruster lifetime assessment to thruster throttling /
    by Van Noord, Jonathan L.
    Published 2010
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    Government Document Conference Proceeding eBook
  11. 11
    Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators /
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    Government Document Conference Proceeding eBook
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