Liquid Rocket Engine : (Record no. 34060)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04967nam a22004453i 4500 |
| 001 - CONTROL NUMBER | |
| control field | EBC28983864 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MiAaPQ |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20240724115756.0 |
| 006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS | |
| fixed length control field | m o d | |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION | |
| fixed length control field | cr cnu|||||||| |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240724s2018 xx o ||||0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9780768095425 |
| Qualifying information | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Canceled/invalid ISBN | 9780768093322 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (MiAaPQ)EBC28983864 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (Au-PeEL)EBL28983864 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC)1130680055 |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | MiAaPQ |
| Language of cataloging | eng |
| Description conventions | rda |
| -- | pn |
| Transcribing agency | MiAaPQ |
| Modifying agency | MiAaPQ |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER | |
| Classification number | TL782 .R494 2019 |
| 082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.475 |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Nardi Rezende, Rene. |
| 245 10 - TITLE STATEMENT | |
| Title | Liquid Rocket Engine : |
| Remainder of title | Thrust Chamber Parametric Modeling. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Warrendale : |
| Name of producer, publisher, distributor, manufacturer | SAE International, |
| Date of production, publication, distribution, manufacture, or copyright notice | 2018. |
| 264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | ©2018. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 1 online resource (158 pages) |
| 336 ## - CONTENT TYPE | |
| Content type term | text |
| Content type code | txt |
| Source | rdacontent |
| 337 ## - MEDIA TYPE | |
| Media type term | computer |
| Media type code | c |
| Source | rdamedia |
| 338 ## - CARRIER TYPE | |
| Carrier type term | online resource |
| Carrier type code | cr |
| Source | rdacarrier |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Cover -- Table of contents -- Acknowledgments -- Nomenclature -- CHAPTER 1 Introduction -- 1.1 Background -- 1.2 Work Objectives -- 1.3 Scope of the Work -- 1.4 Comments on the Project Life Cycle -- 1.5 Parametric Modeling Basics -- References -- CHAPTER 2 Fundamentals of Rocket Propulsion -- 2.1 Introduction -- 2.2 The Main References: A Historical Perspective -- 2.3 Parametric Modeling Application Review -- 2.4 What Is Jet Propulsion? -- 2.5 The de Laval Nozzle -- 2.6 Thrust Equation -- 2.7 Standard Atmosphere -- References -- CHAPTER 3 Methodology -- 3.1 Project Flowchart -- 3.2 High-Level Requirements -- 3.3 Combustion Gases Properties -- 3.3.1 Mixture Ratio -- 3.3.2 Adiabatic Flame Temperature -- 3.3.3 Molar Mass -- 3.3.4 Specific Heats Ratio -- 3.3.5 Sources of Data -- 3.4 Propellant Properties -- 3.4.1 Fuels -- 3.4.2 Oxidizers -- References -- CHAPTER 4 Thrust Chamber Performance Assessment -- 4.1 A Parameter for Thrust Chamber Performance Assessment -- 4.2 Conditions for an Ideal Thrust Chamber -- 4.3 Theoretical Performance -- 4.4 Correction Factors -- 4.5 Validations -- References -- CHAPTER 5 Nozzle Dimensioning -- 5.1 Throat Section Dimensioning -- 5.1.1 Throat Section Dimensioning: First Method -- 5.1.2 Throat Section Dimensioning: Second Method -- 5.2 Exhaust Section Dimensioning -- 5.2.1 Exhaust Section Dimensioning: First Method -- 5.2.2 Exhaust Section Dimensioning: Second Method -- 5.3 When Nozzle Operates Out of the Optimal Point -- 5.4 Validations -- References -- CHAPTER 6 Combustion Chamber Dimensioning -- 6.1 Introduction -- 6.2 Combustion Chamber Volume -- 6.3 Combustion Chamber Diameter -- 6.4 Combustion Chamber Length -- 6.5 Chamber Wall Thickness -- 6.6 Model Assessment -- 6.7 Validations -- References -- CHAPTER 7 Nozzle Configuration -- 7.1 Introduction -- 7.2 Conical Nozzle -- 7.3 Parabolic Nozzle -- 7.4 Validation. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | References -- CHAPTER 8 Complementing the Performance Calculation -- 8.1 Propellant Consumption -- 8.2 Nozzle Flow Equations -- 8.3 Validations -- References -- CHAPTER 9 The Cold Section -- 9.1 Introduction -- 9.2 Impinging Jets -- 9.3 Shower Head -- 9.4 Swirl, Pressure Swirl, or Spray -- 9.5 Pintle -- References -- CHAPTER 10 The Simplex Swirl Injector -- 10.1 Introduction -- 10.2 Swirl Injection Operation -- 10.3 Problem Statement -- 10.4 The Outlet Orifice -- 10.5 The Inlet Orifices -- 10.6 Sizing Methodology -- 10.7 Validation -- References -- CHAPTER 11 The Pintle Injector -- 11.1 Introduction -- 11.2 General Characteristics -- 11.3 Qualitative Analyses: Flow Visualization -- 11.4 Quantitative Analyses: Design Parameters -- 11.5 Validation -- 11.5.1 The 1000-N Injector -- 11.5.2 Validation: The 5000-N Injector -- References -- CHAPTER 12 Appendix -- 12.1 Ground Test -- 12.1.1 Testing a Complete Engine - Hot Test -- 12.1.2 Testing the Propellant Injector - Cold Test -- 12.2 Propellants Charts -- 12.2.1 Liquid Oxygen and Ethanol -- 12.2.2 Liquid Oxygen and Kerosene -- 12.2.3 Liquid Oxygen and Liquid Methane -- 12.2.4 Liquid Oxygen and Liquid Hydrogen -- 12.2.5 Hydrogen Tetroxide and UDMH -- References -- About the Author -- Index. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | Presents an innovative parametric model applicable to the project of some elements of the liquid rocket thrust chamber with the level of detail and accuracy appropriate to the preliminary design phase. |
| 588 ## - SOURCE OF DESCRIPTION NOTE | |
| Source of description note | Description based on publisher supplied metadata and other sources. |
| 590 ## - LOCAL NOTE (RLIN) | |
| Local note | Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Space vehicles-Propulsion systems. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Rockets (Aeronautics). |
| 655 #4 - INDEX TERM--GENRE/FORM | |
| Genre/form data or focus term | Electronic books. |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Print version: |
| Main entry heading | Nardi Rezende, Rene |
| Title | Liquid Rocket Engine |
| Place, publisher, and date of publication | Warrendale : SAE International,c2018 |
| International Standard Book Number | 9780768093322 |
| 797 2# - LOCAL ADDED ENTRY--CORPORATE NAME (RLIN) | |
| Corporate name or jurisdiction name as entry element | ProQuest (Firm) |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=28983864">https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=28983864</a> |
| Public note | Click to View |
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