Advanced Airbreathing Propulsion Cycles For High Speed Flight

881202

8/1/1988

Authors
Abstract
Content
Sustained high speed flight cannot be achieved by improvements in traditional turbojet/turbofan propulsion systems. Instead, propulsion cycles optimized for high speed flight are required. These include combined cycles such as the air turboramjet for the lower speed regime, and scramjet-type cycles for the higher speed regime. Characteristics of these advanced airbreathing propulsion cycles are discussed, and propulsion-related technology issues are addressed.
Meta TagsDetails
DOI
https://doi.org/10.4271/881202
Citation
Campbell, J., Kissinger, R., and Kors, D., "Advanced Airbreathing Propulsion Cycles For High Speed Flight," 1988 Conference and Exposition on Future Transportation Technology, San Francisco, California, United States, August 8, 1988, https://doi.org/10.4271/881202.
Additional Details
Publisher
Published
8/1/1988
Product Code
881202
Content Type
Technical Paper
Language
English