A rocket or ballistic launch rotary wing air vehicle may include a rocket or ballistic launch propulsion system for launching the vehicle, a rotary wing flight system for providing powered flight comprising dual counter rotating coaxial rotors, and a control system programmed to adjust the pitch of a rotor to anyh determined degree of pitch independently of a flap angle of the flap hinge during a transition of the dual counter rotating coaxial rotors from a stowed position to a deployed position.
ROCKET OR BALLISTIC LAUNCHED ROTARY WING UNMANNED AIR VEHICLE
UNBEMANNTES DREHFLÜGELUFTFAHRZEUG FÜR RAKETEN- ODER GESCHOSSABSCHUSS
AÉRONEF SANS PILOTE À VOILURE TOURNANTE À LANCÉMENT BALLISTIQUE OU PAR FUSÉE
2018-02-21
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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