Missile Design Guide.

• Author: Fleeman, Eugene L.
• Place / Publishing House: Reston : : American Institute of Aeronautics & Astronautics,, 2022.; Ã2022.
• Year of Publication: 2022
• Edition: 1st ed.
• Language: English
• Physical Description: 1 online resource (485 pages)

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...

Table of Contents

• 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.
• 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.
• 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.