Draft:Milkor 380

Submission declined on 2 February 2024 by DoubleGrazing (talk).

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Declined by DoubleGrazing 3 months ago. Last edited by Yeieh 3 months ago. Reviewer: Inform author.

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The Milkor 380 is a Medium-altitude long-endurance (MALE) unmanned aerial vehicle (UAV), developed by the South African company Milkor.^[1]

Specifications[edit]

General characteristics[edit]

Length: 9 m
Wingspan: 18 m
Empty Weight: 1300 kg
Fuel capacity: 315 kg
Payload: 220 kg
Powerplant: 1 x four-stroke, four-cylinder turbocharged Rotax 915 iS^[2]

Performance[edit]

Maximum speed: 250 km/h
Cruise speed: 110-150 km/h
Range: 4000 km
Endurance: 30 hr
Service ceiling: 30,000 ft
Operational altitude: 10,000 ft^[1]

References[edit]

^ ^a ^b "Milkor air systems". www.milkor.com/air-system/. Retrieved 2 February 2024.
^ "Milkor 380 UAV makes maiden flight". Retrieved 2 February 2024.

https://www.janes.com/defence-news/news-detail/milkor-380-uav-makes-maiden-flight

[Milkor_air_systems-1] "Milkor air systems". www.milkor.com/air-system/. Retrieved 2 February 2024.

[Milkor_380_UAV_makes_maiden_flight-2] "Milkor 380 UAV makes maiden flight". Retrieved 2 February 2024.

[1]

[2]