This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Use of Thrust Vectoring and Reversing on the S/MTD
Annotation ability available
Sector:
Language:
English
Abstract
A main objective of the STOL and Maneuver Technology Demonstrator, (S/MTD) Program was to evaluate the operability and performance of its unique engine/nozzle configuration which can deliver thrust in three different modes; conventional, vectored and through variable vanes which give the option of going from forward to reverse thrust. The two-dimensional nozzle and the modified engine were extensively tested during sea level and altitude testing to satisfy all flight clearance requirements. This paper concentrates on the flight test results of the various modes of vectoring and reversing ending with a compilation of the actual usage of the propulsive controls that could be used by designers of similar advanced propulsion systems.
Authors
Topic
Citation
Laughrey, J., "Use of Thrust Vectoring and Reversing on the S/MTD," SAE Technical Paper 911173, 1991, https://doi.org/10.4271/911173.Also In
References
- Bursey, R. Dickinson, R. “Flight Test Results of the F-15 SMTD Thrust Vectoring/Thrust Reversing Exhaust Nozzle,” July 1990
- Laughrey, J.A. “Evolution of the STOL and Maneuver Technology Demonstrator,” SAE Paper 872417 November 1987
- Moorhouse, D.J. “Status of the STOL and Maneuver Technology Demonstrator Flight Test Program,” 90 3306 September 1990
- Clough, B.T. “Short Takeoff and Landing Maneuver Technology Demonstrator (STOL/MTD) Lessons Learned: Integrated Flight/Propulsion Control (IFPC),” 90 3307 September 1990
- Lewis, G.V. “F-15 S/MTD Thrust Vectoring/Reversing Flight Test Results,” SAE Aerotech 90 Long Beach, CA October 1990
- Walker, L.A. Jenschke, E.B. Jr. “F-15 STOL/Maneuvering Technology Demonstrator: Phase III: Thrust Vectoring, Reversing and STOL Operations,” SETP 34th Annual Symposium September 1990
- Blake, W.B. “F-15 SMTD Low Speed Jet Effects Wind Tunnel Test Results,” Proceedings of NASA Ames Research Center Workshop on Ground Effects April 1987