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Searched for: 1 subject found.
16.50 Aerospace Propulsion
(
)
Prereq: 16.003 and (2.005 or 16.004)
Units: 3-0-9
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.
C. Guerra Garcia, E.M. Greitzer, J. Sabnis
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