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Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design (Progress in Astronautics and Aeronautics)
December 30, 2004, AIAA (American Institute of Aeronautics & Ast
Hardcover
in English
1563472236 9781563472237
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Book Details
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."
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