The Hybrid Fan Vectored Thrust Engine
831496
10/03/1983
- Event
- Content
- A propulsion system concept with particular application to supersonic short takeoff and vertical landing (STOVL) fighter/attack aircraft has been developed. The concept comprises a variable cycle engine, combining the advantages of a vectored thrust turbofan for takeoff, landing, and subsonic flight with those of a mixed augmented turbofan for high performance and supersonic flight. The system incorporates features and characteristics which have proved both practical and successful on the AV-8 (Harrier), and is potentially an attractive solution.
- Pages
- 12
- Citation
- Ward, B., and Penrose, C., "The Hybrid Fan Vectored Thrust Engine," SAE Technical Paper 831496, 1983, https://doi.org/10.4271/831496.