MIT / Engineering

EVA and Robotics on the Shuttle

By Jeffrey Hoffman | Aircraft Systems Engineering Lecture 20 of 22

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Lecture Description

Course Description

This course 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.

Course Index

  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 + 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
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