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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    Title :

    Rocket Engine Nozzle Concepts


    Contributors:

    Published in:

    Publication date :

    2004-01-01


    Size :

    31 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English



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