Missile Configuration Design
Author | : S. S. Chin |
Publisher | : |
Total Pages | : 304 |
Release | : 1961 |
Genre | : Guided missiles |
ISBN | : |
Beskriver principperne i f.m. konstruktionen af styrede missiler.
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Author | : S. S. Chin |
Publisher | : |
Total Pages | : 304 |
Release | : 1961 |
Genre | : Guided missiles |
ISBN | : |
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Author | : S S Chin |
Publisher | : Hassell Street Press |
Total Pages | : 0 |
Release | : 2023-07-18 |
Genre | : |
ISBN | : 9781019357446 |
This essential guide to missile configuration design provides a detailed overview of the key concepts and techniques involved in designing effective missile systems. Written by a leading expert in the field, this book is an invaluable resource for anyone involved in the design or development of missile systems. This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author | : Eugene L. Fleeman |
Publisher | : |
Total Pages | : |
Release | : 2022 |
Genre | : Astronautics |
ISBN | : 9781624106187 |
"The handbook consists of full color figures with self-standing graphs, tables, charts, and diagrams. It is aimed toward the needs of missile engineers, system engineers, system analysts, program managers, aerospace engineering students, and professors. Readers have a quick reference for missile design, missile technologies, launch platform integration, targeting, fire control integration, missile system measures of merit, and the missile system development process. Topics discussed include: key drivers in the missile design, development, and system engineering process; critical tradeoffs, methods, and technologies in aerodynamic, propulsion, structure, seeker, warhead, fuzing, and subsystems sizing to meet flight performance and other requirements; launch platform and fire control system integration; robustness, lethality, guidance, navigation and control, accuracy, observables, survivability, safety, reliability, and cost considerations; missile sizing examples; missile system and missile technology development process"--
Author | : Eugene L. Fleeman |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 298 |
Release | : 2001 |
Genre | : Technology & Engineering |
ISBN | : |
This is the first textbook offered for tactical missile design. It is oriented toward the needs of aerospace engineering students, missile engineers, and missile program managers. It is intended to provide a basis for including tactical missile design as part of the aerospace engineering curriculum, providing new graduates with the knowledge they will need in their careers. The author's decades of experience in the development of tactical missiles and their technologies is presented in an integrated handbook method for missile design. It uses simple closed-form analytical expressions that are physics-based to provide insight into the primary driving parameters. The text also provides example calculations of rocket-powered and ramjet-powered baseline missiles, typical values of missile parameters, examples of the characteristics of current operational missiles, discussion of the enabling subsystems and technologies of tactical missiles, and the current/projected state of the art of tactical missiles. Included with the text is a CD-ROM containing electronic versions of the figures; 15 videos showing examples of loading missiles, pilot actions, flight trajectories, countermeasures, etc.; and configuration sizing methods.
Author | : Eugene L. Fleeman |
Publisher | : AIAA Education |
Total Pages | : 0 |
Release | : 2012 |
Genre | : Technology & Engineering |
ISBN | : 9781600869082 |
"In his latest book, Missile Design and System Engineering, Eugene L. Fleeman comprehensively reviews the missile design and system engineering process, drawing on his decades of experience in designing and developing missile systems. Addressing the needs of aerospace engineering students and professors, systems analysts and engineers, and program managers, the book examines missile design, missile technologies, launch platform integration, missile system measures of merit, and the missile system development process. This book has been adapted from Fleeman's earlier title, Tactical Missile Design, Second Edition, to include a greater emphasis on system engineering." --Back cover.
Author | : Joseph J. Jerger |
Publisher | : |
Total Pages | : 648 |
Release | : 1960 |
Genre | : Automatic control |
ISBN | : |
Author | : A Atay Tan L |
Publisher | : LAP Lambert Academic Publishing |
Total Pages | : 168 |
Release | : 2011-09 |
Genre | : |
ISBN | : 9783846505823 |
The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques.