Draft:ADASI JERNAS-M

Unmanned aerial vehicle developed in the United Arab Emirates From Wikipedia, the free encyclopedia

The ADASI JERNAS-M is a medium-altitude long-endurance (MALE) unmanned aerial vehicle developed by ADASI, a subsidiary of the UAE-based EDGE Group. According to its manufacturer, it is a tactical multi-mission UAV intended for intelligence, surveillance, reconnaissance, and ground-attack roles.[1]


TypeMedium-altitude long-endurance unmanned aerial vehicle
National originUnited Arab Emirates
Designer
ADASI
Quick facts ADASI JERNAS-M, General information ...
ADASI JERNAS-M
File:JERNAS-M at IDEX 2025.jpg
ADASI JERNAS-M displayed at an exhibition
General information
TypeMedium-altitude long-endurance unmanned aerial vehicle
National originUnited Arab Emirates
ManufacturerADASI
Designer
ADASI
StatusIn development
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File:JERNAS-M at IDEX 2025.jpg
ADASI JERNAS-M on display.

Design

According to EDGE Group, the JERNAS-M is a fixed-wing UAV with a maximum takeoff weight of 1,200 kg, a wingspan of 10 m, and a maximum payload of 280 kg. The company states that it can carry electro-optical, radar, and electronic warfare systems, as well as guided munitions including the RASH MK81 bomb carrying four RASH-3 munitions.[1][2]

EDGE states that the aircraft has an endurance of up to 20 hours in ISR configuration and 12 hours with maximum payload, with a line-of-sight range of 200 km and a maximum speed of 240 km/h.[1][2]

Development

The JERNAS-M was publicly listed by EDGE Group among its air-platform products by 2026.[3] Publicly available manufacturer information as of April 2026 describes the aircraft's intended role and technical characteristics, although detailed independent reporting on its test history, procurement status, and operational use remains limited.[1][2]

Specifications

The following specifications are based on manufacturer-published material.[1][2]

  • Crew: Unmanned
  • Role: MALE tactical multi-mission UAV
  • Wingspan: 10 m
  • Empty weight: 590 kg
  • Maximum takeoff weight: 1,200 kg
  • Payload: 280 kg
  • Fuel capacity: 350 L
  • Maximum speed: 240 km/h
  • Endurance: 20 hours (ISR), 12 hours (maximum payload)
  • Range: 200 km line-of-sight

See also

References

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