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Modern engineering for design of liquid-propellant rocket engines

Author: Dieter K Huzel; David H Huang; Harry Arbit
Publisher: Washington, D.C. : American Institute of Aeronautics and Astronautics, 1992.
Series: Progress in astronautics and aeronautics, v. 147.
Edition/Format:   eBook : Document : EnglishView all editions and formats
Database:WorldCat
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Huzel, Dieter K.
Modern Engineering for Design of Liquid-Propellant Rocket Engines.
Reston : American Institute of Aeronautics and Astronautics, ©2000
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Dieter K Huzel; David H Huang; Harry Arbit
ISBN: 9781600864001 1600864007
OCLC Number: 774285670
Notes: "Sponsored by the Rocketdyne Division of Rockwell International."
Description: 1 online resource (425 pages) : illustrations.
Contents: ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""Table of Contents""; ""Chapter 1. Introduction to Liquid-Propellant Rocket Engines""; ""1.1 Basic Elements of a Liquid-Propellant Rocket Engine""; ""1.2 Generation of Thrust""; ""1.3 Gas-Flow Processes in the Combustion Chamber and Nozzle""; ""The Perfect Gas Law""; ""Principle of Conservation of Energy""; ""Principle of Conservation of Matter""; ""The Isentropic Flow Process""; ""Gas Flow Through Liquid-Propellant Rocket Combustion Chambers""; ""Gas Flow Through Rocket Nozzles"" ""1.4 Performance Parameters of a Liquid-Propellant Rocket Engine""""Thrust-Chamber Specific Impulse (I[sub(s)])tc""; ""Characteristic Velocity c*""; ""Thrust Coefficient C[sub(f)]""; ""Summary of the Influence of pa, ε, γ, R, and (p[sub(c)])ns on Engine Performance""; ""Correction Factors and Magnitudes of Engine Performance Parameters""; ""1.5 Liquid Propellants""; ""Monopropellants""; ""Bipropellants""; ""Cryogenic Propellants""; ""Storable Liquid Propellants""; ""Additives for Liquid Propellants""; ""Optimum Mixture Ratio""; ""Density Impulse""; ""Selection of Liquid Propellants"" ""Liquid-Propellant Performance and Physical Properties""""Chapter 2. Engine Requirements and Preliminary Design Analyses""; ""2.1 Introduction""; ""2.2 Major Rocket-Engine Design Parameters""; ""Thrust Level""; ""Performance""; ""Duration""; ""Mixture Ratio""; ""Weight""; ""Envelope (Size)""; ""Reliability""; ""Cost""; ""Availability (Scheduling)""; ""2.3 Mission Requirements""; ""Typical Mission Goals""; ""Typical Vehicle Requirement Optimization""; ""2.4 Engine Preliminary Design""; ""Engine System and Component Concepts""; ""Preliminary Design Optimization""; ""2.5 Design Philosophy"" ""The Importance of Design Quality""""Systems Analysis and Design Layout""; ""Stress Analysis""; ""Selection of Materials""; ""Chapter 3. Introduction to Sample Calculations""; ""3.1 Approach""; ""3.2 A-1 Stage Engine""; ""General Engine-System Description""; ""System Operation""; ""3.3 A-2 Stage Engine""; ""General Engine-System Description""; ""System Operation""; ""Starting Sequence""; ""Cutoff Sequence""; ""3.4 A-3 Stage Engine""; ""General Engine-System Description""; ""System Operation""; ""3.5 A-4 Stage Engine""; ""General Engine System Description""; ""System Operation"" ""Chapter 4. Design of Thrust Chambers and Other Combustion Devices""""4.1 Basic Thrust-Chamber Elements""; ""4.2 Thrust-Chamber Performance Parameters""; ""Specific Impulse I[sub(s)] (s)""; ""Characteristic Velocity c* (ft/s)""; ""Thrust Coefficient C[sub(f)] (Dimensionless)""; ""Performance Calculation""; ""4.3 Thrust-Chamber Configuration Layout""; ""Combustion-Chamber Volume""; ""Combustion-Chamber Shape""; ""Nozzle Expansion Area Ratio""; ""Nozzle Shape""; ""Clustered-Nozzle Concepts""; ""Alternate Solution""; ""4.4 Thrust-Chamber Cooling""; ""Cooling Techniques and Selection""
Series Title: Progress in astronautics and aeronautics, v. 147.
Responsibility: Dieter K. Huzel and David H. Huang ; revised, updated, and enlarged by Harry Arbit [and others].

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