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MIT16.885JEngineeringundergraduate· 2005

Aircraft Systems Engineering (The Space Shuttle)

Prof. Jeffrey Hoffman & Aaron Cohen

Systems engineering case study of the Space Shuttle taught by NASA's former Space Shuttle program manager and astronauts: main engines, thermal protection tiles, avionics, aerodynamics, and Columbia/Challenger lessons.

Start Lecture 122 lectures · 40h total
Syllabus progress0 of 22 watched
MIT 16.885J: Aircraft Systems Engineering (The Space Shuttle)

Syllabus

22
Lecture 1· 1:50:18

The Origins of the Space Shuttle (MIT 16.885J Aircraft Systems Engineering, Lecture 1)

This lecture introduces the complex systems engineering challenges of the Space Shuttle program, examining its historical genesis, design evolution, and the interplay of technological and programmatic constraints.

Lecture 2· 1:50:23

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

This lecture details the historical development and operational challenges of the Space Shuttle program, providing a case study in large-scale aerospace systems engineering and design iteration.

Lecture 3· 1:51:36

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

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.

Lecture 4· 1:52:52

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

This lecture from MIT's Aircraft Systems Engineering course examines the complex political, economic, and technical considerations that informed the decision to proceed with the Space Shuttle program.

Lecture 5· 1:57:46

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

This lecture details the structural design of the Space Shuttle Orbiter, focusing on its complex airframe and the critical Thermal Protection System. It examines the engineering principles behind ablative and reusable surface insulation materials.

Lecture 6· 1:59:51

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

This lecture from MIT's Aircraft Systems Engineering course details the operational principles and design specifications of the Space Shuttle Main Engines, analyzing their complex turbomachinery and combustion cycles.

Lecture 7· 1:50:23

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

This lecture explores the fundamental principles of aerodynamics, covering regimes from subsonic to hypersonic flight, with an emphasis on their implications for aircraft and spacecraft system design. It details the complex physics governing flight performance across varied velocity profiles.

Lecture 8· 1:53:28

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

This lecture details the design and operational considerations for aircraft landing and mechanical systems, with a focus on principles of structural integrity, hydraulic power, and control mechanisms relevant to aerospace engineering.

Lecture 9· 1:51:17

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

This lecture delves into critical Space Shuttle subsystems, detailing the operation of Orbital Maneuvering Systems (OMS) and Reaction Control Systems (RCS). It also examines the engineering principles behind fuel cells, auxiliary power units, and hydraulic systems essential for flight.

Lecture 10· 1:03:03

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

This session explores the intricate relationship between the Department of Defense (DoD) and the Space Shuttle program, analyzing the strategic and operational requirements that influenced its design and mission profile. It discusses dual-use capabilities and policy implications.

Lecture 11· 1:53:08

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

This lecture dissects the dynamic utilization of Space Shuttle subsystems across various flight phases, from launch and ascent to orbit, reentry, and landing. It illustrates how specific systems are activated and managed to meet changing mission demands.

Lecture 12· 1:55:28

Lecture 12: Aerothermodynamics (16.885J)

This lecture focuses on the fundamental principles of aerothermodynamics as applied to the Space Shuttle, particularly during reentry. It covers heat transfer mechanisms, shockwave phenomena, and thermal protection systems crucial for safe atmospheric flight.

Lecture 13· 1:52:28

Lecture 13: Environmental Control Systems (16.885J)

This session examines the Environmental Control Systems (ECS) of the Space Shuttle, detailing mechanisms for atmosphere revitalization, temperature and humidity control, and waste management. It highlights the engineering challenges of sustaining human life in space.

Lecture 14· 1:48:07

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

This lecture provides an in-depth look at the complex ground operations required for launching the Space Shuttle, from vehicle assembly and payload integration to countdown procedures and launch commit criteria. It covers the intricate logistics and engineering coordination involved.

Lecture 15· 1:50:34

Lecture 15: Space Shuttle Accidents (16.885J)

This lecture critically analyzes major Space Shuttle accidents, including Challenger and Columbia, examining their root causes through detailed engineering and procedural failure analyses. It discusses lessons learned and subsequent changes in safety protocols and design.

Lecture 16· 1:48:49

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

This session elucidates the sophisticated Guidance, Navigation, and Control (GNC) systems of the Space Shuttle. It covers inertial navigation principles, digital flight control algorithms, and sensor fusion techniques that enable precise orbital maneuvers and atmospheric flight.

Lecture 17· 2:00:38

Lecture 17: Mission Control 1 (16.885J)

This lecture provides an overview of the Space Shuttle's Mission Control Center operations, detailing the roles and responsibilities of flight controllers and the command infrastructure. It explores real-time monitoring, communication protocols, and decision-making processes.

Lecture 18· 1:48:54

Lecture 18: Mission Control 2 (16.885J)

Building on the previous session, this lecture further explores the advanced functionalities and emergency procedures implemented in Space Shuttle Mission Control. It focuses on contingency planning, anomaly resolution, and crew-ground interaction strategies.

Lecture 19· 1:49:43

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

This lecture analyzes the iterative design process employed for the Space Shuttle, from conceptualization and preliminary design to detailed engineering and verification. It highlights the challenges of integrating complex systems under stringent performance requirements.

Lecture 20· 1:41:37

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

This session investigates Extravehicular Activity (EVA) procedures and the role of robotics, including the Canadarm, aboard the Space Shuttle. It covers spacesuit technologies, crew training, and the operational utility of robotic manipulators for satellite deployment and maintenance.

Lecture 21· 1:52:08

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

This lecture focuses on the systems engineering principles applied to Space Shuttle payloads, addressing integration requirements, safety protocols, and operational constraints for diverse scientific and commercial missions. It discusses managing interfaces and mission-specific adaptations.

Lecture 22· 1:51:12

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

This session recounts the rigorous test flight program for the Space Shuttle, detailing approach and landing tests (ALT), orbital flight tests (OFT), and their critical role in validating design performance. It covers data acquisition, flight envelope expansion, and pilot feedback.