Specifications

• Wing Span 8.0 m  26.0 ft
• Length 6.0 m  19.6 ft
• Max. Take-off Weight 240.0 kg  530.0 lb
• Max. Payload Weight 35.0 kg  88.0 lb
• Fuel Tank Capacity 90.0 lt

Flight Performance

• Max. Horizontal Speed 180.0 km/h  100.0 kt
• Cruise Speed 120.0 km/h  65.0 kt
• Ceiling 5,000 m  16,000 ft
• Endurance 8~10.0 hr
• Operational Radius 200+ km (Live Video)
• Maximum Range 1,200 km (One way)

Payload

• EO/IR Sensor

Features

• Fully autonomous operation with auto navigation
• Pre-planned Mission capability with runtime mission alteration facility
• MR-UAV is designed for STOL operations on a semi prepared runway
• Conventional wheel landing with provision of emergency parachute system
• Auto Take-off with computer assisted landing
• All composite carbon and glass epoxy reinforced structure
• Line replacement unit architecture of the UAV, providing easy field maintenance
• Capability to accommodate third party FLIR/Mini SAR Payloads
• Operated by a multi-console GCS using custom designed control & navigation software with auto-tracking antenna system
• Extendable Operational Radius by using Multiple GCS configuration
• Reconnaissance, border surveillance, battle damage assessment, search and rescue and various other civil applications