Abstract
The task of propulsion technology concept selection and integration is one of the most challenging problems in aerospace systems design. This is because of the tightly-coupled and inherently multidisciplinary nature of the problem, as well as the multitude of performance constraints and requirements placed on modern propulsion systems. In addition, as the cost of developing new and improved propulsion systems continues to rise, the attendant risk to the developer increases also. This leads to an aversion to risk that stifles innovation, particularly when it involves the
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