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20240329122006.0 |
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|a TL545
|b .H89 1992eb
|
| 082 |
0 |
4 |
|a 629.47522
|
| 049 |
|
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|a UAMI
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| 100 |
1 |
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|a Huzel, Dieter K.
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| 245 |
1 |
0 |
|a Modern engineering for design of liquid-propellant rocket engines /
|c Dieter K. Huzel and David H. Huang ; revised, updated, and enlarged by Harry Arbit [and others].
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| 260 |
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|a Washington, D.C. :
|b American Institute of Aeronautics and Astronautics,
|c 1992.
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| 300 |
|
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|a 1 online resource (425 pages) :
|b illustrations
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| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a computer
|b c
|2 rdamedia
|
| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a Progress in astronautics and aeronautics,
|x 0079-6050 ;
|v v. 147
|
| 500 |
|
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|a "Sponsored by the Rocketdyne Division of Rockwell International."
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| 504 |
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|a Includes bibliographical references and index.
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| 546 |
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|a English.
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| 505 |
0 |
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|a 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
|
| 505 |
8 |
|
|a 1.4 Performance Parameters of a Liquid-Propellant Rocket EngineThrust-Chamber Specific Impulse (I[sub(s)])tc -- Characteristic Velocity c* -- Thrust Coefficient C[sub(f)] -- Summary of the Influence of pa, Îæ, 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
|
| 505 |
8 |
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|a Liquid-Propellant Performance and Physical PropertiesChapter 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
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| 505 |
8 |
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|a The Importance of Design QualitySystems 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
|
| 505 |
8 |
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|a Chapter 4. Design of Thrust Chambers and Other Combustion Devices4.1 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
|
| 590 |
|
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 650 |
|
0 |
|a Liquid propellant rocket engines
|x Design and construction.
|
| 700 |
1 |
|
|a Huang, David H.,
|d 1920-
|1 https://id.oclc.org/worldcat/entity/E39PBJbH3g6T7C9JtRWtDp6kDq
|
| 700 |
1 |
|
|a Arbit, Harry.
|
| 758 |
|
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|i has work:
|a Modern engineering for design of liquid-propellant rocket engines (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGKYP78y4GHfkCYwqkdh9C
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|a Huzel, Dieter K.
|t Modern Engineering for Design of Liquid-Propellant Rocket Engines.
|d Reston : American Institute of Aeronautics and Astronautics, ©2000
|z 9781563470134
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 147.
|x 0079-6050
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111494
|z Texto completo
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| 938 |
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