Advanced Airbreathing Propulsion Cycles For High Speed Flight

881202

08/01/1988

Event
1988 Conference and Exposition on Future Transportation Technology
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
Pages
8
Citation
Campbell, J., Kissinger, R., and Kors, D., "Advanced Airbreathing Propulsion Cycles For High Speed Flight," SAE Technical Paper 881202, 1988, https://doi.org/10.4271/881202.
Additional Details
Publisher
Published
Aug 1, 1988
Product Code
881202
Content Type
Technical Paper
Language
English