Missile Design Guide.
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...
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Place / Publishing House: | Reston : : American Institute of Aeronautics & Astronautics,, 2022. Ã2022. |
Year of Publication: | 2022 |
Edition: | 1st ed. |
Language: | English |
Online Access: | |
Physical Description: | 1 online resource (485 pages) |
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LEADER | 06344nam a22004453i 4500 | ||
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001 | 50029275814 | ||
003 | MiAaPQ | ||
005 | 20240229073849.0 | ||
006 | m o d | | ||
007 | cr cnu|||||||| | ||
008 | 240229s2022 xx o ||||0 eng d | ||
020 | |a 9781624106347 |q (electronic bk.) | ||
020 | |z 9781624106187 | ||
035 | |a (MiAaPQ)50029275814 | ||
035 | |a (Au-PeEL)EBL29275814 | ||
035 | |a (OCoLC)1321800176 | ||
040 | |a MiAaPQ |b eng |e rda |e pn |c MiAaPQ |d MiAaPQ | ||
050 | 4 | |a UG1310 | |
082 | 0 | |a 623.4/519 | |
100 | 1 | |a Fleeman, Eugene L. | |
245 | 1 | 0 | |a Missile Design Guide. |
250 | |a 1st ed. | ||
264 | 1 | |a Reston : |b American Institute of Aeronautics & Astronautics, |c 2022. | |
264 | 4 | |c Ã2022. | |
300 | |a 1 online resource (485 pages) | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a computer |b c |2 rdamedia | ||
338 | |a online resource |b cr |2 rdacarrier | ||
505 | 0 | |a 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 | |a 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 | |a 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 | |a 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 | |a Description based on publisher supplied metadata and other sources. | ||
590 | |a 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 | |a Tactical missiles--Design and construction. | |
650 | 0 | |a Astronautics--Systems engineering. | |
655 | 4 | |a Electronic books. | |
776 | 0 | 8 | |i Print version: |a Fleeman, Eugene L. |t Missile Design Guide |d Reston : American Institute of Aeronautics & Astronautics,c2022 |z 9781624106187 |
797 | 2 | |a ProQuest (Firm) | |
856 | 4 | 0 | |u https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=29275814 |z Click to View |