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
  • Target drone dropping up to 280 kg (617 lbs)
  • 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
Runway length, not less than 850 m (touchdown accuracy - 250 m)
Runway width, not less than 25m (touchdown accuracy - 10 m)
Takeoff and landing on runway Fully automatic
Ground support equipment Not required

 

SPECIFICATIONS

Parameters Data
Wingspan 15 m (49.2 ft)
Length 6.6 m (21.65 ft)
Height 1.7 m (5.57 ft)
Wing area 12.26 m2 (132 ft2)
Gliding ratio 18.3
Empty weight 370 kg (815 lbs)
MTOW 850 kg (1873 lbs)
Fuel capacity 350 l (92 gal)
Max payload 280 kg (617 lbs)
Parachute Ballistic

 

Performance

Parameters Data
Cruising speed (75% power) 200 km/h (124 mi/h)
Range distance 5400 km (3355 mi) with 30 min reserves
Endurance (std tanks) 28 hours
Service ceiling 8,000 m (26246 ft)
Max load factor permitted (x 1.8) +4 g - 2 g
Fuel consum. at cruis. speed 12.4 l/hour (3.35 gl/h)
Engine ROTAX 912IS
Generator 3kW - 12V

 

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