Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design
- 14h 31m
- James Hulka, Michael Popp, Mohammed Habiballah, Vigor Yang
- AIAA
- 2004
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.
In this Book
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Propellant Injection Systems and Processes
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Design and Dynamics of Jet and Swirl Injectors
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Atomization in Coaxial-Jet Injectors
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Liquid Bipropellant Injectors
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Distortion and Disintegration of Liquid Streams
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Modeling Liquid-Propellant Spray Combustion Processes
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Liquid-Propellant Droplet Vaporization and Combustion
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Subcritical/Supercritical Droplet Cluster Behavior in Dense and Dilute Regions of Sprays
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Fundamentals of Supercritical Mixing and Combustion of Cryogenic Propellants
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CARS Measurements at High Pressure in Cryogenic LOX/GH2 Jet Flames
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Propellant Ignition and Flame Propagation
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Rocket Engine Nozzle Concepts
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Nozzle Design and Optimization
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Simulation and Analysis of Thrust Chamber Flowfields—Storable Propellant Rockets
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Simulation and Analysis of Thrust Chamber Flowfields—Storable Propellant Rockets
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Scaling Techniques for Design, Development, and Test
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Assessment of Thrust Chamber Performance
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Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines
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Tripropellant Engine Technology for Reusable Launch Vehicles
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Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications
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Supporting Materials
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