MAE 4161

MAE 4161

Course information provided by the Courses of Study 2014-2015.

A survey in contemporary space technology from satellite subsystem design through launch and mission operations, focusing on the classical subsystems of robotic and human-rated spacecraft, rockets, planetary rovers, and habitats, and with an emphasis on issue of spacecraft-system architecture and design. Topics covered include subsystem technologies and the systems-engineering principles that tie them together into a spacecraft architecture. Subsystem technologies discussed include communications, thermal subsystems, structure, guidance/navigation/control, spacecraft power, space propulsion, payloads (remote sensing, insitu sensing, human life support), entry/descent/landing, surface mobility, and flight-computer hardware and software. The final project consists of architecting a complete spacecraft system with appropriate subsystems, with designs supported by parametric analysis and simulation. Discussions of current problems and trends in spacecraft operation and development. Students will report expectations in a space-system design project in a senior design report.

When Offered Spring.

Prerequisites/Corequisites Prerequisites: MAE 3260 and either MAE 3060 or MAE 4060, or permission of instructor.

Satisfies Requirement Fulfills M.E. Senior Design  requirement.

Comments Co-meets with MAE 4160 and MAE 5160.

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Syllabi: none
  •   Regular Academic Session.  Combined with: MAE 4160MAE 5160

  • 4 Credits Graded