Drag
img not found
Emargency Call

8801711871696

img not found

KAMARKURI 380 SPECIFICATIONS

KAMARKURI 380 SPECIFICATIONS

img not found

SYSTEM CAPABILITIES

MILKOR has independently developed the 380 System to specifically support the integration of the following to its ISR (Intelligence, Surveillance and Reconnaissance) system capabilities:







  • 1. ISR, COMINT and SIGINT Payload Integration
  • 2. Mission System and Sensor Fusion
  • 3. Communications and Networking Systems
  • 4. Computing Solutions
  • 5. Simulators
  • 1. Mission Payload Control
  • 2. Manual and Full Autonomous flight Capability
  • 3. Manual and Full Autonomous
  • 4. Line of Sight Communications (LOSCom)
  • 5. Satellite Communications (SatCom)
  1. 1. Synthetic Aperture Radar (SAR)
  2. 2. Inverse Synthetic Aperture Radar (ISAR)
  3. 3. EO/IR Gimble
  4. 4. Optional Integration of Customer Intelligence Payloads
  5. 5. Brake assisted for ground control
  6. 6. ITAR FREE

MILKOR 380 SPECIFICATIONS

Kamarkuri’s Aerospace team consists of highly skilled engineers, designers and a manufacturing team that can provide turnkey UAS solutions according to user requirements. Milkor currently offers multiple fixed-wing platforms fully equipped for tactical surveillance and opportunistic engagement.



Maximum Range

4000+ km

Maximum Endurance

30 h

Max Operational Altitude

30 000 ft

Line of Sight Communications

250 km (Radius)

Length

9 m

Wingspan

18 m

MTOW

1 500 kg

Maximum Payload

220 kg

Fuel Capacity

315 kg

Maximum Speed

250 km/h

Operational Speed

110–150 km/h

Fuel Type

100 LL AVGAS / 95 MOGAS


Our Products