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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...
| Autor principal: | |
|---|---|
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston :
American Institute of Aeronautics & Astronautics,
2022.
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| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000nam a2200000Mu 4500 | ||
|---|---|---|---|
| 001 | EBOOKCENTRAL_on1321800176 | ||
| 003 | OCoLC | ||
| 005 | 20240329122006.0 | ||
| 006 | m o d | ||
| 007 | cr ||||||||||| | ||
| 008 | 220528s2022 xx o ||| 0 eng d | ||
| 040 | |a EBLCP |b eng |c EBLCP | ||
| 020 | |a 9781624106347 | ||
| 020 | |a 162410634X | ||
| 035 | |a (OCoLC)1321800176 | ||
| 082 | 0 | 4 | |a 623.4/519 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Fleeman, Eugene L. | |
| 245 | 1 | 0 | |a Missile Design Guide |h [electronic resource]. |
| 260 | |a Reston : |b American Institute of Aeronautics & Astronautics, |c 2022. | ||
| 300 | |a 1 online resource (485 p.) | ||
| 500 | |a Description based upon print version of record. | ||
| 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 | |
| 505 | 8 | |a 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 | |
| 505 | 8 | |a 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 | |
| 505 | 8 | |a 3.10 Ramjet Inlet Design Considerations -- 3.11 Ramjet Combustor Design Considerations -- 3.12 Ramjet Booster Integration -- 3.13 Ramjet Inlet Options -- 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 | |
| 505 | 8 | |a 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 | |
| 500 | |a 4.10 Missile Structure Design. | ||
| 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. | ||
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 776 | 0 | 8 | |i Print version: |a Fleeman, Eugene L. |t Missile Design Guide |d Reston : American Institute of Aeronautics & Astronautics,c2022 |z 9781624106187 |
| 856 | 4 | 0 | |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=29275814 |z Texto completo |
| 938 | |a ProQuest Ebook Central |b EBLB |n EBL29275814 | ||
| 994 | |a 92 |b IZTAP | ||