Note 1: We have worked on these UAVs as a dedicated team.
Note 2: Several aircraft with weight classes in different configurations (fixed wing, VTOL etc.,) ranging from 1.0 kg to 1500 kg have been designed. Below are some examples of UAVs with successful flight tests along with their technical specifications (Additional technical information on the aircraft is classified.). The rest of the aircraft information is available upon request.
Ref.: VTOL Aviation
UAV Type: VTOL+Fixed wing (19 kg)
Wing span: 3m
Cruise speed: 23.47 m/s at 5 km
Endurance = 1hr
Flight Test
Ref.: VTOL Aviation
Ref.: Karman Drones
UAV Type: VTOL (tri copter tilt-rotor)+Fixed + Fixed Win (9 kg)
Wing span: 3.2 m
Cruise speed: 19 m/s at 0km and 23.47 m/s at 4 km
Endurance = 2hrs
Flight Test
Ref.: Karman Drones
Ref.: Aerosys Aviation
UAV Type: Fixed wing (7 kg)
Wing span: 2.5 m
Cruise speed: 16 m/s at 5 km
Endurance = 2hrs
Flight Test
Ref.: Aerosys Aviation
Ref.: SpaceJam
UAV Type: Tandem Wing wing (6 kg)
Wing span: 2.5 m
Cruise speed: 15 m/s at Mean Sea Level
Endurance = 1.0 hrs
Flight Test
Ref.: SpaceJam
Ref.: VTOL Aviation
UAV Type: Flying wing (3 kg)
Wing span: 2 m
Cruise speed: 13 m/s at Mean Sea Level
Endurance = 0.5 hr
Flight Test
Ref.: VTOL Aviation
UAV Type: Fixed wing (25 kg)
Wing span: 4.3 m
Cruise speed: 23.47 m/s at 5 km
Endurance = 6hrs
UAV Type: Fixed wing (22 kg)
Wing span: 3 m
Cruise speed: 30.70 m/s at 5 km
Endurance: =24 hrs