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  1. 1
    Test devices for aeronautical research and technology

    Test devices for aeronautical research and technology

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  2. 2
    Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft

    Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft by Richard, Jacques C.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  3. 3
    Characteristics of ions emitted from high-current hollow cathodes

    Characteristics of ions emitted from high-current hollow cathodes by Kameyama, Ikuya

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  4. 4
    Propulsion over a wide Mach number range

    Propulsion over a wide Mach number range by Resler, Edwin L.

    Ithaca, NY : [Washington, DC] : [Springfield, Va.] : Cornell University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


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  5. 5
    The NASA on-board propulsion program

    The NASA on-board propulsion program by Curran, Francis M.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  6. 6
    Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system

    Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system by Georgiadis, Nicholas J.

    [Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor, 1999
    Format: Government Document Book


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  7. 7
    Supersonic reacting internal flow fields

    Supersonic reacting internal flow fields by Drummond, J. Philip

    [Washington, D.C.?] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


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  8. 8
    Unsteady ejector performance : an experimental investigation using a pulsejet driver

    Unsteady ejector performance : an experimental investigation using a pulsejet driver by Paxson, Daniel E.

    Cleveland, Ohio : Hanover Md. :; Cleveland, Ohio : Hanover MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for AeroSpace Information, 2002
    Format: Government Document Book


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  9. 9
    Assessment of High Temperature Superconducting (HTS) electric motors for rotorcraft propulsion

    Assessment of High Temperature Superconducting (HTS) electric motors for rotorcraft propulsion by Doernbach, Jay

    [Washington, D.C.] :; [Washington, D.C.] : National Aeronautics and Space Administration, 1990
    Format: Government Document Book


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  10. 10
    Effects of slag ejection on solid rocket motor performance

    Effects of slag ejection on solid rocket motor performance

    Washington, D.C. : [Springfield, Va.] : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  11. 11
    Electrodynamic tether propulsion and power generation at Jupiter

    Electrodynamic tether propulsion and power generation at Jupiter

    [Huntsville, Ala.] : Springfield, VA : National Aeronautics and Space Administration, Marshall Space Flight Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


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  12. 12
    SRM internal flow test and computational fluid dynamic analyses : final report : contract NAS8-39095

    SRM internal flow test and computational fluid dynamic analyses : final report : contract NAS8-39095

    Huntsville, Alabama : [Washington, DC] : [Springfield, Va.] : ERC, Inc. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  13. 13
    NSTAR ion thruster plume impacts assessments

    NSTAR ion thruster plume impacts assessments

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  14. 14
    NASA Lewis Propulsion Systems Laboratory customer guide manual

    NASA Lewis Propulsion Systems Laboratory customer guide manual by Soeder, Ronald H.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  15. 15
    Computational fluid dynamics study of the variable-pitch split-blade fan concept

    Computational fluid dynamics study of the variable-pitch split-blade fan concept by Kepler, C. E.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  16. 16
    Performance tests of a liquid hydrogen propellant densification ground system for the X33/RLV

    Performance tests of a liquid hydrogen propellant densification ground system for the X33/RLV by Tomsik, Thomas M.

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  17. 17
    Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

    Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 by Capone, Francis J.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  18. 18
    Overview of space propulsion systems identifying nondestructive evaluation and health monitoring opportunities

    Overview of space propulsion systems identifying nondestructive evaluation and health monitoring opportunities by Generazio, Edward R.

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  19. 19
    A synopsis of ion propulsion development projects in the United States : SERT I to Deep Space I

    A synopsis of ion propulsion development projects in the United States : SERT I to Deep Space I by Sovey, J. S.

    [Cleveland, Ohio] : [Springfield, Va.] :; [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


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  20. 20
    Performance of a quasi-steady, multi megawatt, coaxial plasma thruster

    Performance of a quasi-steady, multi megawatt, coaxial plasma thruster

    [Cleveland, Ohio] : [Springfield, Va.] : Lewis Research Center, National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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