Missile Design Guide. (Record no. 34400)
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| fixed length control field | 06372nam a22004573i 4500 |
| 001 - CONTROL NUMBER | |
| control field | EBC29275814 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MiAaPQ |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20240724115806.0 |
| 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 | 240724s2022 xx o ||||0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781624106347 |
| Qualifying information | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Canceled/invalid ISBN | 9781624106187 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (MiAaPQ)EBC29275814 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (Au-PeEL)EBL29275814 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC)1321800176 |
| 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 | UG1310 |
| 082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 623.4/519 |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Fleeman, Eugene L. |
| 245 10 - TITLE STATEMENT | |
| Title | Missile Design Guide. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Reston : |
| Name of producer, publisher, distributor, manufacturer | American Institute of Aeronautics & Astronautics, |
| Date of production, publication, distribution, manufacture, or copyright notice | 2022. |
| 264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | ©2022. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 1 online resource (485 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 -- Half Title -- Title Page -- Copyright Page -- Contents -- Preface -- Chapter 1: Introduction -- 1.1 Overview -- 1.2 Missile Characteristics Comparison -- 1.3 Conceptual Design and System Engineering Process -- 1.4 System-of-Systems Comparison -- 1.5 Examples of State-of-the-Art Missiles -- 1.6 Examples of Alternatives in Establishing Mission Requirements -- 1.7 Use of a Baseline Missile -- Chapter 2: Aerodynamics -- 2.1 Introduction -- 2.2 Missile Diameter Tradeoff -- 2.3 Nose Fineness and Geometry Tradeoffs -- 2.4 Body Drag Prediction -- 2.5 Boattail Tradeoffs -- 2.6 Body Normal Force and Lift-to-Drag Prediction -- 2.7 Sign Convention of Forces, Moments, and Axes -- 2.8 Static Stability and Body Aerodynamic Center Prediction -- 2.9 Flare Stabilizer Tradeoffs -- 2.10 Wings Versus No Wings -- 2.11 Normal Force Prediction for Planar Surfaces -- 2.12 Aerodynamic Center Location and Hinge Moment Prediction for Planar Surfaces -- 2.13 Planar Surface Drag and Lift-to-Drag Prediction -- 2.14 Surface Planform Geometry and Integration Alternatives -- 2.15 Flight Control Alternatives -- 2.16 Maneuver Law Alternatives -- 2.17 Roll Angle and Control Surface Sign Convention -- 2.18 Trim and Static Stability Considerations -- 2.19 Stability and Control Conceptual Design Criteria -- Chapter 3: Propulsion -- 3.1 Introduction -- 3.2 Propulsion Alternatives Assessment -- 3.3 Turbojet Flow Path, Components, and Nomenclature -- 3.4 Turbojet Thrust Prediction -- 3.5 Turbojet Specific Impulse Prediction -- 3.6 Subsonic Turbojet Propulsion Efficiency -- 3.7 Ramjet Flow Path, Components, and Nomenclature -- 3.8 Ramjet Temperature and Specific Impulse Prediction -- 3.9 Ramjet Thrust Prediction -- 3.10 Ramjet Inlet Design Considerations -- 3.11 Ramjet Combustor Design Considerations -- 3.12 Ramjet Booster Integration -- 3.13 Ramjet Inlet Options. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | 3.14 Supersonic Inlet/Airframe Integration -- 3.15 Fuel Alternatives -- 3.16 Solid Propellant Rocket Motor Flow Path, Components, and Nomenclature -- 3.17 Rocket Motor Performance Prediction -- 3.18 Rocket Motor Sizing Process -- 3.19 Solid Propellant Rocket Motor Production Alternatives -- 3.20 Solid Propellant Rocket Thrust Magnitude Control -- 3.21 Solid Propellant Alternatives -- 3.22 Solid Propellant Aging -- 3.23 Solid Propellant Rocket Combustion Stability -- 3.24 Rocket Motor Case and Nozzle Material Alternatives -- 3.25 Ducted Rocket Design Considerations -- Chapter 4: Weight -- 4.1 Introduction -- 4.2 Missile Weight Prediction -- 4.3 Center-of-Gravity and Moment-of-Inertia Prediction -- 4.4 Missile Airframe Structure Manufacturing Processes -- 4.5 Missile Airframe Material Alternatives -- 4.6 Missile Structure/Insulation Trades -- 4.7 H igh Temperature Insulation Materials -- 4.8 Missile Aerodynamic Heating/Thermal Response Prediction -- 4.9 Localized Aerodynamic Heating and Thermal Stress -- 4.10 Missile Structure Design -- 4.11 Seeker Dome Alternatives -- 4.12 Missile Power Supply and Flight Control Actuators -- Chapter 5: Flight Performance -- 5.1 Introduction -- 5.2 Missile Flight Performance Envelope -- 5.3 Equations of Motion Modeling -- 5.4 Driving Parameters for Missile Flight Performance -- 5.5 Steady-State Flight and Constant Bearing Intercept -- 5.6 Boost, Glide, Coast, Ballistic, and Divert Flight -- 5.7 Turn Performance -- Chapter 6: Other Measures of Merit -- 6.1 Introduction -- 6.2 Robustness -- 6.3 Lethality -- 6.4 Accuracy -- 6.5 Carriage and Launch Observables -- 6.6 Missile Survivability and Safety -- 6.7 Reliability -- 6.8 Cost -- 6.9 Launch Platform/Fire Control Integration -- Chapter 7: Sizing Examples and Sizing Tools -- 7.1 Introduction -- 7.2 Rocket Baseline Missile -- 7.3 Ramjet Baseline Missile. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | 7.4 T urbojet Baseline Missile -- 7.5 Baseline Guided Bomb -- 7.6 Computer Aided Conceptual Design Sizing Tools -- 7.7 Soda Straw Rocket (DBF, Pareto, Uncertainty Analysis, HOQ, DOE) -- Chapter 8: Development Process -- 8.1 Missile Technology and System Development Process -- 8.2 E xamples of State-of-the-Art Advancement -- 8.3 Enabling Technologies for Missiles -- Chapter 9: Lessons Learned -- Chapter 10: Summary -- 10.1 Missile Design Guidelines -- 10.2 Wrap Up -- Chapter 11: References, Bibliography -- 11.1 References -- 11.2 Bibliography -- Chapter 12: Appendices -- List of Figures -- Follow-up Communication -- Index -- Supplemental Materials. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | In his latest book, Missile Design Guide, Eugene Fleeman presents a comprehensive compilation of the missile design process pulling from his 50+ years of experience in the design and development of missile systems. The handbook consists of full color figures with self-standing graphs, tables, charts, and diagrams. |
| 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 | Tactical missiles--Design and construction. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Astronautics--Systems engineering. |
| 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 | Fleeman, Eugene L. |
| Title | Missile Design Guide |
| Place, publisher, and date of publication | Reston : American Institute of Aeronautics & Astronautics,c2022 |
| International Standard Book Number | 9781624106187 |
| 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=29275814">https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=29275814</a> |
| Public note | Click to View |
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