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.
Nozzle Design and Optimization
Liquid Rocket Thrust Chambers ; 469-492
2004-01-01
24 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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