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.
Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications
Liquid Rocket Thrust Chambers ; 683-701
2004-01-01
Article/Chapter (Book)
Electronic Resource
English
Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications
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