THE DEVELOPMENT OF PROP-ROTOR SYSTEM FOR 52KG MTOW QUAD-TILT PROP (QTP) UAV
European Rotorcraft Forum ; 45. ; 2019 ; Warschau
2020
Conference paper
English
DEMONSTRATION OF PROP-ROTOR SYSTEM DEVELOPMENT FOR 52KG MTOW QUAD-TILT PROP UAV
British Library Conference Proceedings | 2020
|Tilt Prop-Rotor Composite Research Aircraft
NTIS | 1968
|