
Liquid Rocket Thrust Chambers
Aspects of Modeling, Analysis, and Design
American Institute of Aeronautics & Astronautics (Publisher)
Published on 31. October 2004
Book
Hardback
500 pages
978-1-56347-223-7 (ISBN)
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 countriesChina, France, Germany, Italy, Japan, the Netherlands, Russia, Sweden, and the United States.
More details
Language
English
Place of publication
Reston
United States
Target group
College/higher education
Professional and scholarly
Product notice
sewn/stitched
Paper over boards
Illustrations
Illustrations
Dimensions
Height: 247 mm
Width: 155 mm
Thickness: 44 mm
Weight
1104 gr
ISBN-13
978-1-56347-223-7 (9781563472237)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Classification
Content
Injection and Atomization; Propellant Injection Systems and Processes; Dynamics of Liquid Rocket Injectors; Atomization of Coaxial-Jet Injectors; Atomization of Impinging-Liquid Jets; Disintegration and Distortion of Liquid Streams; Combustion and Ignition; Modeling of Liquid-Propellant Combustion in Rocket Engine Combustor; Liquid-Propellant Droplet Vaporization and Combustion; Droplet Cluster Behavior in Dense and Dilute Regions of Sprays; Supercritical Combustion; CARS Measurements in Cryogenic LOX-GH2 Jet Flames; Propellant Ignition and Flame Propagation; Nozzle Concepts, Design, and Optimization; Rocket Engine Nozzle Concepts; Nozzle Design and Optimization; Thrust Chamber Dynamics, Heat Transfer, and Performance; Simulation and Analysis of Thruster Chamber Flowfields: Storable Propellant Rockets; Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic-Propellant Rockets; Scaling Techniques in Liquid Rocket Engine Combustion Devices Testing; Thrust Chamber Cooling and Heat Transfer; Assessment of Thrust Chamber Performance; Aspects of Engine System Design; Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines; Tripropellant Liquid Rocket Engine Technology; Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications