Description This is the first major publication on liquid-rocket combustion devices since 1960, and includes 20 chapters prepared by world-renowned experts. Each chapter focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics, and is incorporated into the volume in a well-organized, cohesive manner. There are contributions from nine different countries--China, France, Germany, Italy, Japan, The Netherlands, Russia, Sweden, and the United States.


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    Titel :

    Tripropellant Engine Technology for Reusable Launch Vehicles


    Beteiligte:
    Popp, Michael (Autor:in) / Hulka, James (Autor:in) / Yang, Vigor (Autor:in) / Habiballah, Mohammed (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.2004




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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    Bell annular tripropellant engine concept

    Vilja, John / Lobitz, James | AIAA | 1994


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    Optimal Control of Gradual Tripropellant Engine for SSTO

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