Overview of Missile Design and System Engineering
8 - 9 March 2015
, Laurel, Maryland
Held in conjunction with:
This course provides an overview of missile design and system engineering. A system-level, integrated method is provided for missile design, technologies, development, analysis, and system engineering activities in addressing requirements such as cost, performance, risk, and launch platform integration. The methods presented are generally simple closed-form analytical expressions that are physics-based, to provide insight into the primary driving parameters. Sizing examples are presented for rocket-powered, ramjet-powered, and turbo-jet powered baseline missiles as well as guided bombs. Typical values of missile parameters and the characteristics of current operational missiles are discussed as well as the enabling subsystems and technologies for missiles and the current/projected state of the art. Videos illustrate missile development activities and performance. Attendees will receive a copy of the course notes.
• Key drivers in the missile propulsion design and system engineering process
• Critical tradeoffs, methods, and technologies in propulsion system sizing to meet flight performance and other requirements
• Launch platform-missile integration
• Sizing examples for missile propulsion
• Missile propulsion system and technology development process
Who Should Attend
The course is oriented toward the needs of missile engineers, system engineers, system analysts, marketing personnel, program managers, university professors, and others working in the area of missile propulsion systems and missile propulsion technology development. Attendees will gain an understanding of missile propulsion design, missile propulsion technologies, launch platform integration, missile propulsion system measures of merit, and missile propulsion system development process.