Thrust vectoring is a key technology for future combat aircraft. Together with an advanced thrust vectored engine control system, the ITP thrust vectoring nozzle concept with a common actuation system for all nozzle functions (throat area, exit area and all axis vectoring) is an appropriate solution to meet the stringent requirements concerning performance, reliability and safety resulting from the intended use of thrust vectoring for flight control. An enhanced link between the flight control system and the engine control system will be necessary and the combined engine and nozzle control will have to meet new functional requirements. These requirements are on one hand related to the nozzle itself and on the other hand to the interactions between the nozzle and the engine.
Integrated Thrust Vectored Engine Control
2001
10 pages
Report
Keine Angabe
Englisch
Aircraft , Rocket Engines & Motors , Military aircraft , Thrust vector control systems , Thrust augmentor nozzles , Kinematics , Functions , Steady state , Control systems , Computations , Jet engines , Limitations , Vector analysis , Germany , Engines , Geometry , Actuators , Combat forces , German language , Miniaturization , Gas flow , Component reports , Foreign reports
The Hybrid Fan Vectored Thrust Engine
SAE Technical Papers | 1983
|History of the Pegasus vectored thrust engine
AIAA | 1981
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