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.
Tripropellant Engine Technology for Reusable Launch Vehicles
Liquid Rocket Thrust Chambers ; 649-682
01.01.2004
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Tripropellant Engine Technology for Reusable Launch Vehicles
British Library Conference Proceedings | 2004
|Tripropellant Combustion Investigation
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|Bell annular tripropellant engine concept
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|Bell Annular Tripropellant Engine Concept
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|Optimal Control of Gradual Tripropellant Engine for SSTO
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