Lectures (Video)
- 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
Space Shuttle Systems Engineering - Lecture 11
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Lecture 11 - Use of Subsystems as a Function of Flight Phase
Prof. Jeffrey Hoffman, Prof. Aaron Cohen
16.885J / ESD.35J Aircraft Systems Engineering, Fall 2005 (Massachusetts Institute of Technology: MIT OpenCourseWare) http://ocw.mit.edu Date accessed: 2009-11-24 License: Creative Commons BY-NC-SA |