Present study deals with the study on the effect of Nytrox oxidizer which is the combination of both gaseous oxygen and gaseous nitrous oxide with the wax as a fuel on regression rate, combustion efficiency, and sliver loss. The oxygen was injected through the axial or showerhead injector, and for the nitrous oxide, two different injectors were used, i.e., radial and swirl injector. The study had been carried out with three different combinations of the N2O and oxygen, i.e., 50:50, 70:30, 80:20 ratio. It was further compared with the GOX and N2O. It has been observed that the pure N2O gave lower regression rate compared to the oxygen unless swirl injector was used with N2O. Among the injectors used, most effective in enhancing performance was swirl, then the radial and last was the showerhead injector. Among the combination of all the three oxidizers used, the 50:50 ratio was the most promising in all respect of performance improvement.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Use of N2O–O2 as the Oxidizer for the Hybrid Rocket Application


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Sivaramakrishna, Gullapalli (Herausgeber:in) / Kishore Kumar, S. (Herausgeber:in) / Raghunandan, B. N. (Herausgeber:in) / Kumar, Rajiv (Autor:in) / Thamizarasan, K. (Autor:in)


    Erscheinungsdatum :

    2022-07-24


    Format / Umfang :

    17 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Variable-flow hybrid rocket oxidizer injector

    Robertson, David / Mueller, Paul | AIAA | 2001


    A numerical investigation of oxidizer mixed hybrid rocket motors

    Chidambaram, Palani Kumar | Online Contents | 2015



    Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection

    Paccagnella, Enrico / Karabeyoglu, Arif M. / Barato, Francesco et al. | AIAA | 2015


    A numerical investigation of oxidizer mixed hybrid rocket motors

    Chidambaram, Palani Kumar / Kumar, Amit | Elsevier | 2015