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16.50 Aerospace Propulsion

Prereq: 16.003; 16.004 or 2.005
U (Spring)
12 Units

Presents aerospace propulsive devices as systems, with functional requirements and engineering and environmental limitations. Requirements and limitations that constrain design choices. Both air-breathing and rocket engines covered, at a level which enables rational integration of the propulsive system into an overall vehicle design. Mission analysis, fundamental performance relations, and exemplary design solutions presented.

S. Barrett, J. Sabnis

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Aerospace Engineering (Course 16)

Degree Chart for Bachelor of Science in Aerospace Engineering (Course 16)

School of Science

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