Performance parameters of power-limited propulsion systems are expressed formally in terms of kinematic properties of thrust units; ion engine deficiencies, such as neutral efflux, multiple ionization, and propellant stream divergence, are described as velocity distributions in exhaust stream and related algebraically to important mission parameters; background is provided for selection of best set of physical measurements to be made for evaluation of thrust units; it is shown how these measurements are related to mission parameters.


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    Titel :

    Evaluation and analysis of thrust units for power-limited propulsion systems


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Shelton, R.D. (Autor:in) / Potter, R.A. (Autor:in) / Lacy, L. (Autor:in) / Stuhlinger, E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 4


    Erscheinungsdatum :

    1964


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Evaluation and analysis of thrust units for power-limited propulsion systems

    Lacy, L. / Potter, R. A. / Shelton, R. D. et al. | NTRS | 1964


    Evaluation and analysis of thrust units for powerlimited propulsion systems

    LACY, L. / POTTER, R. A. / SHELTON, R. D. et al. | AIAA | 1964


    Trajectory Optimization With Dual Thrust Limited Propulsion Systems

    Ocampo, C. A. / Rosborough, G. W. / American Astronautical Society et al. | British Library Conference Proceedings | 1997


    Lateral Thrust Units and Manoeuvring Propulsion Devices

    Gokarn, R. P. | Springer Verlag | 2024


    Trajectory Optimization With Dual Thrust Limited Propulsion Systems (AAS 01-443)

    Ocampo, C. / AAS / AIAA | British Library Conference Proceedings | 2001