Design Process as it Relates to the Shuttle

1. The Origins of the Space Shuttle
2. Space Shuttle History
3. Orbiter Sub-System Design
4. The Decision to Build the Shuttle
5. Orbiter Structure and Thermal Protection System
6. Propulsion - Space Shuttle Main Engines
7. Aerodynamics - (From Sub - to Hypersonic and Back)
8. Landing and Mechanical Systems
9. OMS, RCS, Fuel Cells, Auxiliary Power Unit and Hydraulic Systems
10. The DoD and the Space Shuttle
11. Use of Subsystems as a Function of Flight Phase
12. Aerothermodynamics
13. Environmental Control Systems
14. Ground Operations - Launching the Shuttle
15. Space Shuttle Accidents
16. Guidance, Navigation and Control
17. Mission Control 1
18. Mission Control 2
19. Design Process as it Relates to the Shuttle
20. EVA and Robotics on the Shuttle
21. Systems Engineering for Space Shuttle Payloads
22. Test Flying the Space Shuttle
23. Exemplary Lecture: Shuttle Operations Video

16.885J offers a holistic view of the aircraft as a system, covering: basic systems engineering; cost and weight estimation; basic aircraft performance; safety and reliability; lifecycle topics; aircraft subsystems; risk analysis and management; and system realization. Small student teams retrospectively analyze an existing aircraft covering: key design drivers and decisions; aircraft attributes and subsystems; and operational experience. Oral and written versions of the case study are delivered. For the Fall 2005 term, the class focuses on a systems engineering analysis of the Space Shuttle. It offers study of both design and operations of the shuttle, with frequent lectures by outside experts. Students choose specific shuttle systems for detailed analysis and develop new subsystem designs using state of the art technology. http://ocw.mit.edu