Initial discussion covers aircraft design philosophies, design standards and regulations. In-depth coverage of design specification development. Instruction in design report writing and technical presentations. Aircraft conceptual design development is covered including development of fixed wing aircraft using initial sizing parameters, estimate of maximum take-off weight, wing loading, power loading, aerodynamic coefficients and physical dimensions. A discussion follows on special features of the aircraft and how these issues impact on performance and operational requirements. Students commence the aerospace design and build project during this course.