Rockets & Launch Vehicles: Selection and Design
$2290 per person
This four-day course provides an overview of rockets and missiles, including a fourth day covering advanced selection and design processes. The course provides a wide practical knowledge in rocket and missile issues and technologies. The seminar is designed for engineers, supporting disciplines, decision makers and managers of current and future projects needing a more complete understanding of the complex issues of rocket and missile technology. The seminar provides a foundation for understanding the issues that must be decided in the design, use, regulation, selection and development of rocket systems of the future. You will learn a wide spectrum of problems, solutions and choices in the technology of rockets and missile used for both military and civil purposes. The seminar is taught to the point-of-view of a decision maker needing the technical knowledge to make better informed choices in the multi-discipline world of rockets and missiles. The class provides what you need to know about how rockets and missiles work, why they are build the way they are, what they are used for and how they differ from use to use. You will learn how rockets and missiles differ when used as weapons, as launch vehicles, and in spacecraft or satellites. The objective is to give the decision maker all the tools needed to understand the available choices, and to manage or work with other technical experts of different specialized disciplines. Attendees will receive a 210-page text book by the presenter, covering the course, and a complete set of printed class notes used during the class. The book is a more in-depth and permanent explanation of each slide presented in first three days of the class. These notes, and the book, will be an excellent future reference for anyone in the aerospace business.
What you will learn:
- Fundamentals of rocket and missile systems, functions and disciplines
- The full spectrum of rocket systems, uses and technologies
- Optimum Selection and Design strategies
- Fundamentals and uses of solid, liquid and hybrid rocket systems
- Differences between weapons systems and those built for commerce
Who should attend:
- Engineers, Managers, and Specialists in all aspects of Rocket Design, Fabrication, Operation and Selection.
- Government and Aerospace decision makers
- Those working with, or supporting, Rocket projects and Programs.
- Introduction to Rockets and Missiles – The student is introduced to the historic and practical uses of rocket systems.
- Classifications of Rockets and Missiles – The classifications and terminology of all types of rocket systems are defined.
- Rocket Propulsion made Simple – The chemistry and physics of all rockets and rocket nozzles operate to achieve thrust is explained. Rocket performance modeling is introduced.
- Rocket Flight Environments – The flight environments of rockets, such as acceleration, heating, shock, and vibration, are explored.
- Aerodynamics and Winds – The effect of winds, atmospheric density and velocity on lift, drag, and dynamic pressure is explained. Rocket shape, stability and venting are discussed.
- Performance Analysis and Staging – The use of performance modeling and loss factors, are defined. Staging theory for multi-stage rockets are explained.
- Mass Properties and Propellant Selection – The relative importance of specific impulse, bulk density, bulk temperature, storability, ignition properties, stability, toxicity, operability, material
compatibility, and ullege are defined. Monopropellant and cold gas propellants are introduced.
- Introduction to Solid Rocket Motors – The historical and technological aspects of Solid Rocket Motors is explored. Solid rocket materials, propellants, thrust-profiles, construction, cost advantages and special applications are explained.
- Fundamentals of Hybrid Rockets – The technology and Problems of hybrid rockets is discussed.
- Liquid Rocket Engines – Pressure and pump-fed liquid rocket engines are explained, including injectors, cooling, chamber construction, pump cycles, ignition and thrust vector control.
- Introducing the Liquid Rocket Stage – Liquid rocket stages are introduced, including tank systems, pressurization, cryogenics, and other structures
- Thrust Vector Control – Thrust Vector control hardware and alternatives are explained.
- Basic Rocket Avionics – Flight electronics elements of Guidance, Navigation, Control, Communications, Telemetry, Range Safety and Payloads are defined.
- Modern Expendable Launch Vehicles – Good launch vehicle design are defined, with alternative examples.
- Rockets in Spacecraft Propulsion – The differences between systems on spacecraft, satellites and transfer stages, operating in microgravity, are examined.
- Launch Sites and Operations – The role and purpose of launch sites, and the choices available for a launch operations infrastructure, is explored.
- Useful Orbits & Trajectories Made Simple – A simplified presentation of orbital mechanics, for the understanding rocket propulsion in orbital trajectories and maneuvers, is provided.
- Safety of Rocket Systems – The hazards and mitigations of rocket operations are examined.
- Reliability of Rocket Systems – Reliability, and strategies to improve reliability, are discussed, including random and systematic failures, reliability environments, quality, robustness, and redundancy.
- Reusable Launch Vehicle Theory – Why Reusable Launch Vehicles have had difficulty replacing expendable launch vehicles.
- Rocket Cost Principals and Cases – Cost estimation methods modeling systems as a science, including why costs are so high. Strategies from the Soyuz Case illustrate alternatives and to cost reduction. Integrated modeling and incentives are introduced.
- Chemical Rocket Propulsion Alternatives – Alternatives to chemical rocket propulsion includes air breathing, nuclear, thermal, cannons, and tethers are explored.
- Proliferation of Missile Technology – Foreign Rocket threats
- The Future of Rockets and Missiles – The direction of rocket technology, science, usage and regulations is conducted.
- Opportunities to Select and/or Design Optimum Launch Vehicles. – In your career, you may work on selection of Space Mission Launch Vehicles, or work on the design Launch Vehicle, or both. This fourth day will help you understand optimization processes for both the design and selection of Launch Vehicles.
- Selection – The time and circumstances of optimum selection is explored, and the reasons are explained.
- Optimizing the Selection Trade Study Process Standard vs. optimum processes are explained.
- Integrating Available Information on Alternatives All Launch Vehicle characteristics must be accurately determined.
- The Goals and Incentives of Launch Vehicle Design – Setting goals and incentives for a success project. Goals and incentives of the past explain future successes and failures
- Optimum Launch Vehicle Design Strategies – Optimum design strategies are explained to the extent that the student will understand what works and what fails. These strategies are barley understood throughout the Aerospace community, leading to many bad assumptions.
- Understanding Why Good Designs Succeed – The strategies from Soyuz, Delta, Space-X, and beyond, are wrapped up. The student will understand how to optimize both the selection and design process of Launch Vehicles.
If this course is not on the current schedule of open enrollment courses and you are interested in attending this or another course as an open enrollment, please contact us at (410) 956-8805 or email@example.com. Please indicate the course name, number of students who wish to participate. and a preferred time frame. ATI typically schedules open enrollment courses with a 3-5 month lead time. For on-site pricing, you can use the request an on-site quote form, call us at (410) 956-8805, or email us at firstname.lastname@example.org.
Edward L. Keith is a multi-discipline Launch Vehicle System Engineer, specializing in integration of launch vehicle technology, design, modeling and business strategies. He is currently an independent consultant, writer and teacher of rocket system and space mission technology. He is experienced in launch vehicle operations, design, testing, business analysis, risk reduction, modeling, safety and reliability. Mr. Keith’s experience extends to both reusable and expendable launch vehicles, as well as to solid, liquid and hybrid rocket systems. Mr. Keith has designed complete rocket engines, rocket vehicles, small propulsion systems, and composite propellant tank systems, especially designed for low cost. His travels have taken him to Russia, China, Australia and other launch operations centers throughout the world. Mr. Keith has worked the Space Launch Initiative and the Liquid Fly-Back Booster programs for Boeing, originated the Scorpius Program for Microcosm, worked on the Brilliant Eyes and the Advanced Solid Rocket Motor Programs for Rockwell and worked on the Aerojet Launch Detection Satellite program. He also has 13-years of government experience including five years working launch operations at Vandenberg AFB. Mr. Keith has written 22 technical papers and two textbooks on various aspects of space transportation over the last three decades.
Daniel J. Moser, Founder, President and Chief Technical Officer of an engineering consultant firm has a B.S. in Physics, and M.E. in Mechanical Engineering, University of Utah. Mr. Moser has been an engineer, innovator, and entrepreneur in the aerospace industry for over 35 years. Previously employed by Beal Aerospace Technologies (Director of Engineering), Raytheon-Electronic Systems (Chief Composites Engineer), ALCOA-FiberTek (Project Engineer), and EDO-Fiber Science (Project/Test Engineer), he has also founded and operated two composites-based businesses: Utah Rocketry (1993-1997), and Compositex, Inc. (2000-present). He has extensive experience in designing and developing launch vehicles, liquid rocket propulsion systems, ablatively-cooled thrust chambers/nozzles, filament-wound composite vessels (liquid propellant tanks, high-pressure gas storage vessels, solid rocket motorcases, and crash-worthy external aircraft fuel tanks), wings, control surfaces, fuselages, radomes, spars, missile tail fins, bulkheads, reentry heat shields, and landing gear. Compositex, Inc. customers include NASA-Marshall, NASA-Ames, NASA-Johnson, Air Force Research Laboratory, Johns Hopkins University-Applied Physics Laboratory, Air Launch LLC, Blue Origin, Virgin Galactic, KT Engineering, Rocketdyne, DARPA, Exxon-Mobil, Northrop Grumman, and Lockheed Martin.
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