ALBATROSS 2.2

Fixed Wing UAV

Medium Altitude Long Endurance (MALE) UAS with a long flight duration about 25h with 88 lb (40 kg) payload.
Based on the piloted Pipistrel Sinus aircraft.

Overview

The aircraft is designed for long-endurance missions in conditions of high turbulence and overloads.
The reinforced fuselage and landing gear are engineered for harsh landings, including on grass airfields or prepared sites.
Take-off, route flight, and landing are carried out in fully automated mode.
Proprietary Autopilot.
The ALBATROSS UAV is equipped with satellite communication data link for Beyond Line of Sight (BVLOS) operation.
Resistance to jamming.

BENEFITS

  • Low cost of flying hour
  • The reliability of certified devices increases the reliability of the entire UAV system as a whole
  • The availability of a large network of dealer centers and spare parts stores
  • The conversion reduces the production time for an UAV

Application

  • Day and Night operations
  • Cargo delivery
  • Locating poachers and unauthorised activity in National Parks and other wildlife areas
  • All kinds of Surveillance including communications interception
  • Disaster Help – Civilian Support
  • Maritime/Coastal Patrol
  • SAR Operation and Victim discovery

OPERATION SPECIFICATIONS

Parameters Data
Operating temperature -40°C…+40°C (-40 ...104F)
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

 

Submit a Request

Submit a Request

UAVOS

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