The propulsion cycle options for hypersonic vehicles are summarized including airbreathing, rocket and combinations. Each cycle is characterized by configuration, performance, efficiency and operating envelope. The major components of each propulsion system are identified and evaluated for influence on overall performance. Several combined cycle configurations offer the best propulsion characteristics for the various hypersonic missions from hypersonic transport to single stage to orbit. The unique experimental testing requirements for hypersonic propulsion systems present a significant challenge.


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