Missile System DesignCourse # D190February 9-12, 2015Columbia, Maryland$2095 (8:30am - 4:00pm)Register 3 or More & Receive $100 00 EachOff The Course Tuition.SummaryThis four-day short course covers the fundamentals ofmissile design, development, and system engineering. Missilesprovide the essential accuracy and standoff range capabilitiesthat are of paramount importance in modern warfare.Technologies for missiles are rapidly emerging, resulting in thefrequent introduction of new missile systems. The capability tomeet the essential requirements for the performance, cost, andrisk of missile systems is driven by missile design and systemengineering. The course provides a system-level, integratedmethod for missile aerodynamic configuration/propulsiondesign and analysis. It addresses the broad range ofalternatives in meeting cost, performance, and riskrequirements. The methods presented are generally simpleclosed-form analytical expressions that are physics-based, toprovide insight into the primary driving parameters. Typicalvalues of missile parameters and the characteristics of currentoperational missiles are discussed as well as the enablingsubsystems and technologies for missiles and thecurrent/projected state-of-the-art. Daily roundtable discussion.Design, build, and fly competition. Over seventy videosillustrate missile development activities and missileperformance. Attendees will vote on the relative emphasis ofthe material to be presented. Attendees receive course notesas well as the textbook, Missile Design and SystemEngineering.InstructorEugene L. Fleeman has 50 years of government, industry,academia, and consulting experience inMissile Design and System Engineering.Formerly a manager of missile programs atAir Force Research Laboratory, RockwellInternational, Boeing, and Georgia Tech, heis an international lecturer on missiles andthe author of over 100 publications, includingthe AIAA textbook, Missile Design andSystem Engineering.What You Will Learn• Key drivers in the missile design and system engineeringprocess.• Critical tradeoffs, methods and technologies in subsystems,aerodynamic, propulsion, and structure sizing.• Launch platform-missile integration.• Robustness, lethality, guidance navigation & control,accuracy, observables, survivability, safty, reliability, andcost considerations.• Missile sizing examples.• Development process for missile systems and missiletechnologies.• Design, build, and fly competition.Who Should AttendThe course is oriented toward the needs of missileengineers, systems engineers, analysts, marketingpersonnel, program managers, university professors, andothers working in the area of missile systems and technologydevelopment. Attendees will gain an understanding of missiledesign, missile technologies, launch platform integration,missile system measures of merit, and the missile systemdevelopment process.Video!www.aticourses.com/tactical_missile_design.htmCourse Outline1. Introduction/Key Drivers in the Missile System DesignProcess: Overview of missile design process. Examples of system-ofsystemsintegration. Unique characteristics of missiles. Keyaerodynamic configuration sizing parameters. Missile conceptualdesign synthesis process. Examples of processes to establish missionrequirements. Projected capability in command, control,communication, computers, intelligence, surveillance, reconnaissance(C4ISR). Example of Pareto analysis. Attendees vote on courseemphasis.2. Aerodynamic Considerations in Missile System Design:Optimizing missile aerodynamics. Shapes for low observables. Missileconfiguration layout (body, wing, tail) options. Selecting flight controlalternatives. Wing and tail sizing. Predicting normal force, drag,pitching moment, stability, control effectiveness, lift-to-drag ratio, andhinge moment. Maneuver law alternatives.3. Propulsion Considerations in Missile System Design:Turbojet, ramjet, scramjet, ducted rocket, and rocket propulsioncomparisons. Turbojet engine design considerations, prediction andsizing. Selecting ramjet engine, booster, and inlet alternatives. Ramjetperformance prediction and sizing. High density fuels. Solid propellantalternatives. Propellant grain cross section trade-offs. Effective thrustmagnitude control. Reducing propellant observables. Rocket motorperformance prediction and sizing. Solid propellant rocket motorcombustion instability. Motor case and nozzle materials.4. Weight Considerations in Missile System Design: How tosize subsystems to meet flight performance requirements. Structuraldesign criteria factor of safety. Structure concepts and manufacturingprocesses. Selecting airframe materials. Loads prediction. Weightprediction. Airframe and motor case design. Aerodynamic heatingprediction and insulation trades. Dome material alternatives and sizing.Power supply and actuator alternatives and sizing.5. Flight Performance Considerations in Missile SystemDesign: Flight envelope limitations. Aerodynamic sizing-equations ofmotion. Accuracy of simplified equations of motion. Maximizing flightperformance. Benefits of flight trajectory shaping. Flight performanceprediction of boost, climb, cruise, coast, steady descent, ballistic,maneuvering, divert, and homing flight.6. Measures of Merit and Launch Platform Integration:Achieving robustness in adverse weather. Seeker, navigation, datalink, and sensor alternatives. Seeker range prediction. Countercountermeasures.Warhead alternatives and lethality prediction.Approaches to minimize collateral damage. Fuzing alternatives andrequirements for fuze angle and time delay. Alternative guidance laws.Proportional guidance accuracy prediction. Time constant contributorsand prediction. Maneuverability design criteria. Radar cross sectionand infrared signature prediction. Survivability considerations.Insensitive munitions. Enhanced reliability. Cost drivers of schedule,weight, learning curve, and parts count. EMD and production costprediction. Logistics considerations. Designing within launch platformconstraints. Standard launchers. Internal vs. external carriage.Shipping, storage, carriage, launch, and separation environmentconsiderations. Launch platform interfaces. Cold and solarenvironment temperature prediction.7. Sizing Examples and Sizing Tools: Trade-offs for extendedrange rocket. Sizing for enhanced maneuverability. Developing aharmonized missile. Lofted range prediction. Ramjet missile sizing forrange robustness. Ramjet fuel alternatives. Ramjet velocity control.Correction of turbojet thrust and specific impulse. Turbojet missilesizing for maximum range. Turbojet engine rotational speed. Guidedbomb performance. Computer aided sizing tools for conceptual design.Design, build, and fly competition. Pareto, house of quality, and designof experiment analysis.8. Missile Development Process: Design validation/technologydevelopment process. Developing a technology roadmap. History oftransformational technologies. Funding emphasis. Cost, risk, andperformance tradeoffs. New missile follow-on projections. Examples ofdevelopment tests and facilities. Example of technology demonstrationflight envelope. Examples of technology development. Newtechnologies for missiles.20 – Vol. 119 Register online at www.ATIcourses.com or call ATI at 888.501.2100 or 410.956.8805
Modern Missile AnalysisPropulsion, Guidance, Control, Seekers, and <strong>Technology</strong>Course # D193January 19-22, 2015Huntsville, AlabamaFebruary 17-20, 2015Columbia, Maryland$1990 (8:30am - 4:00pm)Register 3 or More & Receive $100 00 EachOff The Course Tuition.SummaryThis four-day course presents a broad introduction tomajor missile subsystems and their integrated performance,explained in practical terms, but including relevant analyticalmethods. While emphasis is on today’s homing missiles andfuture trends, the course includes a historical perspective ofrelevant older missiles. Both endoatmospheric andexoatmospheric missiles (missiles that operate in theatmosphere and in space) are addressed. Missile propulsion,guidance, control, and seekers are covered, and their rolesand interactions in integrated missile operation are explained.The types and applications of missile simulation and testingare presented. Comparisons of autopilot designs, guidanceapproaches, seeker alternatives, and instrumentation forvarious purposes are presented. The course is recommendedfor analysts, engineers, and technical managers who want tobroaden their understanding of modern missiles and missilesystems. The analytical descriptions require some technicalbackground, but practical explanations can be appreciated byall students. U.S. citizenship is required for this course.InstructorDr. Walter R. Dyer is a graduate of UCLA, with a Ph.D.degree in Control Systems Engineering and<strong>Applied</strong> Mathematics. He has over thirty yearsof industry, government and academicexperience in the analysis and design oftactical and strategic missiles. His experienceincludes Standard Missile, Stinger, AMRAAM,HARM, MX, Small ICBM, and ballistic missiledefense. He is currently a Senior StaffMember at the Johns Hopkins University <strong>Applied</strong> PhysicsLaboratory and was formerly the Chief Technologist at theMissile Defense Agency in Washington, DC. He has authorednumerous industry and government reports and publishedprominent papers on missile technology. He has also taughtuniversity courses in engineering at both the graduate andundergraduate levels.What You Will LearnYou will gain an understanding of the design and analysisof homing missiles and the integrated performance of theirsubsystems.• Missile propulsion and control in the atmosphere and inspace.• Clear explanation of homing guidance.• Types of missile seekers and how they work.• Missile testing and simulation.• Latest developments and future trends.Video!www.aticourses.com/missile_systems_analysis.htmCourse Outline1. Introduction. Brief history of Missiles. Types ofmissiles. Introduction to ballistic missile defense.Endoatmospheric and exoatmospheric missiles. Missilebasing. Missile subsystems overview. Warheads, lethality andhit-to-kill. Power and power conditioning.2. Missile Propulsion. Rocket thrust and the rocketequation. Specific impulse and mass fraction. Solid and liquidpropulsion. Propellant safety. Single stage and multistageboosters. Ramjets and scramjets. Axial propulsion. Thrustvector control. Divert and attitude control systems. Effects ofgravity and atmospheric drag.3. Missile Airframes, Autopilots And Control. Purposeand functions of autopilots. Dynamics of missile motion andsimplifying assumptions. Single plane analysis. Missileaerodynamics. Autopilot design. Open-loop and closed loopautopilots. Inertial instruments and feedback. Pitch and rollautopilot examples. Autopilot response, stability, and agility.Body modes and rate saturation. Induced roll in highperformance missiles. Adaptive autopilots. Rolling airframeMissiles. Exoatmospheric Kill Vehicle autopilots. Pulse WidthModulation. Limit cycles.4. Missile Seekers. Seeker types and operation for endoandexo-atmospheric missiles. Passive, active and semiactive seekers. Atmospheric transmission. Strapped downand gimbaled seekers. Radar basics. Radar seekers andmissile fire-control radar. Radar antennas. Sequential lobing,monopulse and frequency agility. Passive sensing basics andinfrared seekers. Figures of merit for detectors. Introduction toseeker optics and passive seeker configurations. Scanningseekers and focal plane arrays. Dual mode seekers. Seekercomparisons and applications to different missions. Signalprocessing and noise reduction.5. Missile Guidance. Phases of missile flight. Boost andmidcourse guidance. Lambert Guidance. Homing guidance.Zero effort miss. Proportional navigation and augmentedproportional navigation. Predictive guidance. Optimumhoming guidance. Homing guidance examples and simulationresults. Gravity bias. Radomes and their effects. Blind range.Endoatmospheric and exoatmospheric missile guidance.Sources of miss and miss reduction. Miss distancecomparisons with different homing guidance laws. Guidancefilters and the Kalman filter. Early guidance techniques. Beamrider, pure pursuit, and deviated pursuit guidance.6. Simulation and Testing. Current simulationcapabilities and future trends. Hardware in the loop. Types ofmissile testing and their uses, advantages and disadvantagesof testing alternatives.Register online at www.ATIcourses.com or call ATI at 888.501.2100 or 410.956.8805 Vol. 119 – 21