ALBATROSS 2.2

The aerodrome based drone
with completely automatic takeoff,
en-route flight and landing

Overview

The reinforced fuselage and the gear of Albatross 2.2 are engineered to endure multiple takeoffs and landings during a day, as well as considerable maneuvering accelerations and high speed.
UAVis converted from a manned Pipistrel Sinus aircraft.
The carrier is made of composite material with low RCS.
Takeoff, en-route flight and landing of the drone are fully automatic. Havihg entered a flight mission into GCU, an operator presses the button to permit takeoff; all next procedures are done automatically.
Diagnostics, flight planning and remote control can be performed using a wireless network connection.
Proprietary Autopilot.

Application

  • Video surveillance and monitoring
  • Payload dropping (up to 100 kg)
  • Payload delivery and autonomous transporting
  • Radio relay
  • R&D flying laboratory (meteorology, hydrology, earth monitoring, etc.)

OPERATIONS SPECIFICATIONS

Parameters Data
Temperature range -40°C…+50°C (-40 ...122F)
Base Paved runway
Takeoff ground roll 132 m (430 ft)
Takeoff total distance over 50 ft obst. 232 m (760 ft)
Landing distance over 50 ft obst. 270 m (885 ft)
Rolling touchdown accuracy range 2-250 m (6.5-820 ft)
Pitch touchdown accuracy 2-10 m (6.5-32 ft)
Runway length, considering the min. touchdown accuracy 770 m (2526 ft)
Runway width, considering the min. touchdown accuracy 25 m (82 ft)
Takeoff and landing on runway Fully automatic
Ground support equipment Not required

 

SPECIFICATIONS

Parameters Data
Wing span 14.97 m (49.1 ft)
Length 6.5 m (21.32 ft)
Height 1.82 m (6 ft)
Cockpit width 1.12 m (44 in)
Aspect ratio 18.3
Empty weight 300 kg (661 lb)
MTOW 550 kg (1210 lb)
Fuel capacity 150 l (40 gal)
Max payload 250 kg (551 lb)
Parachute Ballistic

 

Performance

Parameters Data
Cruising speed (75% power) 205 km/h (127 mi/h)
Range distance 2255 km (1401 mi) with 30 min reserves
Nominal endurance 11 hours, with 30 min reserves
Maximum endurance 20 hours
Service ceiling 7,200 m (23600 ft)
Max load factor permitted (x 1.8) +4 g - 2 g
Fuel consum. at cruise speed 13 l/hour
Engine ROTAX 912IS
Generator 3kW - 12V

 

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