A differential thrust vectoring system including a first thruster rotation assembly configured to rotate a first thruster relative of an aircraft, a second thruster rotation assembly configured to rotate a second thruster of an aircraft, and an actuator. The system is configured such that actuation of the actuator causes disparate rotation about the tilt axis of the first and second thrusters.
Differential thrust vectoring system
2022-05-24
Patent
Elektronische Ressource
Englisch
Thrust vectoring apparatus and flying object having thrust vectoring apparatus
Europäisches Patentamt | 2017
|AIAA | 1970
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