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Liquid Rocket Thrust Chambers (Progress in Astronautics and Aeronautics) [Hardcover]

V. Yang (Author), M. Habiballah (Author), M. Popp (Author), J. Hulka (Author)

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Book Description

January 1, 2005 1563472236 978-1563472237
This is the first major publication on liquid-rocket combustion devices since 1960. A total of 26 chapters prepared by world-renowned experts in their subject areas are included. 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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Liquid Rocket Thrust Chambers (Progress in Astronautics and Aeronautics) + Modern Engineering for Design of Liquid Propellant Rocket Engines (Progress in Astronautics and Aeronautics) + Rocket Propulsion Elements
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Inside This Book (learn more)
First Sentence:
THE liquid propellant combustion device has always presented design and development risks because of the required harsh operating thermal environment, usually at high pressures, and because of the secondary goals of small packaging, light weight, high performance efficiency, and low cost. Read the first page
Key Phrases - Capitalized Phrases (CAPs): (learn more)
Journal of Fluid Mechanics, Physics of Fluids, New York, Proceedings of the Combustion Institute, United States, Jet Propulsion, Canoga Park, Begell House, Chemical Propulsion Information Agency, Senior Member, Mashinostroenie Pub, Final Report, Final Rept, International Journal of Multiphase Flow, Centre National, Chemical Engineering Science, Department of Mechanical Engineering, Marshall Space Flight Center, University Park, Aerojet General Corp, Associate Fellow, Cambridge Univ, European Symposium, Pennsylvania State Univ, Axial Distance From Chamber Throat
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