UAV (Unmanned Aerial Vehicle) WULUNG

UAV Wulung is remotely controlled both manually and automatically. It uses composite materials and powered by pusher type single piston engine and is Equipped with single Ground Control Station as central control. Wulung has a capability to perform ISR (Intelligence, Surveillance and Reconnaissance).

PERFORMANCE

Take-Off ( Sea Level, MTOW )
Take Off Distance : 350 m

Cruise Speed ISA, 800 ft pressure altitude standard atmosphere at gross weight of 125 Kg)
Max. Cruise Speed : 100 KTAS
Operational Speed : 60 KTAS

Landing Distance (ISA, Sea Level Conditions, MLW)
Landing Distance : 350 m
Maximum Endurance : 4 hr
Radius of Operation : 120 km

GEOMETRI

Overall Length : 4.42 m
Overall Height : 1.48 m
Max. Fuselage Width : 0.40 m
Wing Span : 6.34 m
Wheel Base : 1.44 m
Wheel Track : 1.60 m

WEIGHT

Max. Take Off Weight(MTOW) : 125 Kg
Basic Empty Weight : 65 Kg
Max. Fuel : 32 Kg
Max. Payload : 35 Kg
Max. Take Off Weight : 16,000 Kg
Max. Landing Weight : 15,800 Kg
Max. Zero Fuel Weight : 14,900 Kg
Max. Payload : 4,700 Kg
Take Off Run : 404 m
Take Off Distance : 793 m
Landing Roll : 378 m
Landing Distance : 924 m
Maximum Cruise Speed : 237 Kts
Loiter Speed : 168 Kts
Maximum Range : 2,274 NM
Max. Operational Ceiling : 25,000 ft
Range with Max. Payload* : 407 NM
Ferry Range* : 2,237 NM
*With 45 minutes fuel reserve
Engine : Powered by two (2) General Electric CT7-9C with 1,750 SHP each (1,870 SHP with APR).
Propeller : Two (2) four-bladed Hamilton Standard HS 14 RF-21 propellers