Description
Design approach and phases. Design integration. Influence of mission and other requirements on vehicle configuration. Trade-off studies, sizing and configuration layout. Flight vehicle loads, velocity-load factor diagram. Structural design: overall philosophy, role in design process, methods. Basic orbital mechanics; launch vehicle sizing.
Prerequisites
- Prerequisite(s): AERO 2001 .
Conditions and arrangements
- Prerequisite(s): AERO 2001 .
- Lectures three hours a week, problem analysis three hours a week.
Reference text in its original language
Design approach and phases. Design integration. Influence of mission and other requirements on vehicle configuration. Trade-off studies, sizing and configuration layout. Flight vehicle loads, velocity-load factor diagram. Structural design: overall philosophy, role in design process, methods. Basic orbital mechanics; launch vehicle sizing.
- Prerequisite(s): AERO 2001 .
- Lectures three hours a week, problem analysis three hours a week.
Sources and references
Dates and sources are retained to help you verify the information. Translations are provided to facilitate reading; the official source governs conditions and requirements.
Source reference : https://calendar.carleton.ca/undergrad/courses/AERO/