Two kinds of parabolic thrusters with a focal point and a round shroud focus respectively were studied. Numerical and experimental results showed that impulse coupling coefficient Cm was largely dependent on nozzle’s shape. Propulsion performance of laser thruster with a focal point is better than that with a round shroud focus.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Effects of Nozzle Structure on Laser Thruster Performance


    Beteiligte:
    Cui, Cunyan (Autor:in) / Hong, Yanji (Autor:in) / Wen, Ming (Autor:in) / Wang, Jun (Autor:in) / He, Guoqiang (Autor:in) / Komurasaki, Kimiya (Herausgeber:in) / Yabe, Takashi (Herausgeber:in) / Uchida, Shigeaki (Herausgeber:in) / Sasoh, Akihiro (Herausgeber:in)

    Kongress:

    BEAMED ENERGY PROPULSION: Fourth International Symposium on Beamed Energy Propulsion ; 2005 ; Nara (Japan)


    Erschienen in:

    Erscheinungsdatum :

    02.05.2006


    Format / Umfang :

    5 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Effects of Nozzle Structure on Laser Thruster Performance

    Cui, C. / Hong, Y. / Wen, M. et al. | British Library Conference Proceedings | 2006


    NOZZLE PERFORMANCE OF A RP LASER THRUSTER

    Hirooka, Y. / Katsurayama, H. / Mori, K. et al. | British Library Conference Proceedings | 2003


    Nozzle Performance of a RP Laser Thruster

    Hirooka, Yasuro / Katsurayama, Hiroshi / Mori, Koichi et al. | AIAA | 2003


    Computational Analysis on Nozzle Performance of a RP Laser Thruster

    Hirooka, Y. / Katsurayama, H. / Mori, K. et al. | British Library Conference Proceedings | 2004


    Micro-nozzle thruster

    MANZONI GIULIO | Europäisches Patentamt | 2016

    Freier Zugriff