Future space missions are expected to be significantly impacted by developments in hybrid rocket propellant technology. Propellants that are more effective, sustainable, and good for the environment are needed to travel to more places in space and are cost-effective. In the current scenario, it is necessary to use high-performance propellant with the least amount of fuel so that space missions can reach their orbit and accomplished their mission. Sounding rockets, experimental airplanes, and space launch vehicles are just a few of the current uses for hybrid rocket engines. Due to a better combination of fuel/oxidizer and their benefits, such as a high specific impulse, improved safety, and simpler handling compared to conventional liquid or solid fuel rockets, hybrid rockets have the potential to be used in military weapons. The effectiveness of blend metal additions in enhancing the performance of hybrid rocket propellants has been the subject of much investigation. Metal additives can improve mechanical and combustion properties. This paper evaluates fuels such as paraffin and paraffin with additives aluminum and boron and oxidizer as liquid oxygen and discusses their combustion characteristics.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Numerical Studies of Hybrid Rocket Propellant


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Singh, Sanjay (Herausgeber:in) / Ramulu, Perumalla Janaki (Herausgeber:in) / Gautam, Sachin Singh (Herausgeber:in) / Thakur, Amit Kumar (Autor:in) / Nikam, Sanjivani (Autor:in) / Srivastava, Sachin (Autor:in)

    Kongress:

    International Conference on Modern Research in Aerospace Engineering ; 2023 ; Noida, India September 21, 2023 - September 22, 2023



    Erscheinungsdatum :

    2024-04-28


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Some Typical Hybrid Propellant Rocket Motors

    B. T. C. Zandbergen | NTIS | 1995


    Hybrid rocket motor propellant selection alternatives

    ESTEY, PAUL / WHITTINGHILL, GEORGE | AIAA | 1992


    Spray Ignition Studies on a Green Hypergolic Hybrid Rocket Propellant

    Nath, Syamantak / Mallick, Lovely / Lefkowitz, Joseph | TIBKAT | 2023


    Spray Ignition Studies on a Green Hypergolic Hybrid Rocket Propellant

    Nath, Syamantak / Mallick, Lovely / Lefkowitz, Joseph | AIAA | 2023


    Ignition Studies on a Non-Toxic Hypergolic Hybrid Rocket Propellant

    Nath, Syamantak / Laso, Iker / Lefkowitz, Joseph | British Library Conference Proceedings | 2022