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MIT 16.885J: Aircraft Systems Engineering (The Space Shuttle) →0/22
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The Origins of the Space Shuttle (MIT 16.885J Aircraft Systems Engineering, Lecture 1)

1:50:18
2

Space Shuttle History (MIT 16.885J Aircraft Systems Engineering, Lecture 2)

1:50:23
3

Orbiter Sub-System Design (MIT 16.885J Aircraft Systems Engineering, Lecture 3)

1:51:36
4

The Decision to Build the Shuttle (MIT 16.885J Aircraft Systems Engineering, Lecture 4)

1:52:52
5

Orbiter Structure and Thermal Protection System (MIT 16.885J Aircraft Systems Engineering, Lecture 5)

1:57:46
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Propulsion: Space Shuttle Main Engines (MIT 16.885J, Lecture 6)

1:59:51
7

Aerodynamics: Subsonic to Hypersonic Flight (MIT 16.885J Aircraft Systems Engineering, Lecture 7)

1:50:23
8

Landing and Mechanical Systems (MIT 16.885J, Lecture 8)

1:53:28
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Lecture 9: OMS, RCS, Fuel Cells, Auxiliary Power Unit and Hydraulic Systems (16.885J)

1:51:17
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Lecture 10: The DoD and the Space Shuttle (16.885J)

1:03:03
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Lecture 11: Use of Subsystems as a Function of Flight Phase (16.885J)

1:53:08
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Lecture 12: Aerothermodynamics (16.885J)

1:55:28
13

Lecture 13: Environmental Control Systems (16.885J)

1:52:28
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Lecture 14: Ground Operations - Launching the Shuttle (16.885J)

1:48:07
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Lecture 15: Space Shuttle Accidents (16.885J)

1:50:34
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Lecture 16: Guidance, Navigation and Control (16.885J)

1:48:49
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Lecture 17: Mission Control 1 (16.885J)

2:00:38
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Lecture 18: Mission Control 2 (16.885J)

1:48:54
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Lecture 19: Design Process as it Relates to the Shuttle (16.885J)

1:49:43
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Lecture 20: EVA and Robotics on the Shuttle (16.885J)

1:41:37
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Lecture 21: Systems Engineering for Space Shuttle Payloads (16.885J)

1:52:08
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Lecture 22: Test Flying the Space Shuttle (16.885J)

1:51:12

Orbiter Sub-System Design (MIT 16.885J Aircraft Systems Engineering, Lecture 3)

Jeffrey Hoffman & Aaron CohenMIT

Five-Flight NASA Astronaut & Former NASA JSC Director

1:51:36·2008·undergraduate level

This lecture details the critical sub-system design considerations for the Space Shuttle Orbiter, covering architectural choices, component integration, and the engineering challenges inherent in complex spacecraft.

EngineeringAerospace EngineeringSystems DesignSpace ShuttleOrbital Mechanics

Orbiter Sub-System Design

View the complete course: http://ocw.mit.edu/16-885F05

More courses at http://ocw.mit.edu

Previous · Lecture 2

Space Shuttle History (MIT 16.885J Aircraft Systems Engineering, Lecture 2)

Next · Lecture 4

The Decision to Build the Shuttle (MIT 16.885J Aircraft Systems Engineering, Lecture 4)

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