SKELDAR V-200

THE MOST ADVANCED TECHNOLOGIES
AVAILABLE

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Seeing is Believing

Designed for civilian, military and maritime missions, this unmatched Vertical Take-Off & Landing (VTOL) System is truly multi-role, and ideal for a wide range of applications such as Reconnaissance, Identification, Target Acquisition and Electronic Warfare. Equipped with multiple capabilities including surveillance and 3-D mapping, UMS SKELDAR’s UAVs provide an edge in any environment – day or night.

With a double payload capability and uniquely
incorporating Heavy Fuel,
the SKELDAR V-200
is the perfect Unmanned Aerial Vehicle (UAV)
for maritime and naval operations.

The SKELDAR V-200
is maritime ready.

On watch, all the time, real time.

Maritime Ready Plaftorm

Heavy Fuel
Engine

Low life-cycle
costs

STANAG 4586
compliant

Key features:

  • Multiple capabilities in land, civil security and maritime sectors
  • Multiple Payload Capacity
  • Easy Deployment – No Airfield needed
  • Fully Automated Vertical Take-off and Landing (ATOL)
  • Maritime Ready
  • Heavy Fuel Engine
  • Point-and-Fly and Point-and-See principle
  • Tethering Mode supporting moving RPS
  • Single or dual operator setup
  • Redundant flight safety critical components
  • Open interface to BMS and C4ISR system
  • STANAG 4586 compliant
  • ITAR free
SKELDAR V-200

Typical Payload Options

The SKELDAR V-200 is a versatile Vertical Take-Off & Landing (VTOL) solution for a wide range of applications such as Reconnaissance, Identification, Target Acquisition and Electronic Warfare. A number of Commercial Off-The-Shelf (COTS) high resolution Electro Optical/Infrared (EO/IR), Synthetic Aperture Radar (SAR) and Electronic Warfare (EW) sensors are available.

SKELDAR V-200

Technical Specifications

PERFORMANCE:

Payload capacity:
MTOW:
Data Link Range:
Max Airspeed:
Service Ceiling:
Fuel:
Endurance:

Multiple
235 kg (518 lbs)
100 km, 200 km (54 NM, 108 NM)
150 km/h (81 kts)
3000 m (9842 ft)
Heavy Fuel (Jet A-1, JP5, JP8)

5+ hours
Subject to size of fuel tank module
and payload configuration

PHYSICAL:

Rotor diameter:
Airframe lenght:
Height:
Width:

4.6 m (15 ft)
4 m (13 ft)
1.3 m (4.2 ft)
1.2 m (4 ft)