A jet aircraft includes an aircraft integrated, fluid vectoring, exhaust nozzle system. Implementation of this disclosure may eliminate or reduce the size of the aircraft vertical stabilizer and rudder assembly, thereby potentially improving aircraft survivability and increasing aircraft thrust-to-weight ratio.
FLUID-VECTORING SYSTEM
FLUIDVEKTORISIERUNGSSYSTEM
SYSTÈME DE VECTORISATION DE FLUIDE
2020-09-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |