The unique modular design of the SKELDAR V-150 enables ease of transportability and accelerated maintenance. Its small logistical footprint can be halved for transport and storage thanks to an easily removable tail boom and rotor section. Routine engine overhauls and maintenance are carried out efficiently thanks to one easily removable engine and sub-frame Line Replaceable Unit (LRU).
Unmanned Helicopter Designed to Deliver Intelligence & Support Tactical Operations.

System Introduction

Unmanned Helicopter Key Features
Payload Flexibility
SKELDAR V-150
Payload Flexibility


Payload Options
As an agnostic platform, the V-150 is an open architecture to numerous sensor combinations supporting role change payloads. Depending on mission needs, Commercial-Off-The-Shelf (COTS) high-resolution Electro-Optical/Infrared (EO/IR), Synthetic Aperture Radar (SAR), Light Detection and Ranging (LiDAR), Electronic Warfare (EW) sensors and other mission-specific payloads are offered.
Sensors:
- Night & Day Electro-Optical/Infrared (EO/IR) Sensors
Radar & LiDAR options including:
- Synthetic Aperture Radars (SAR)
- Light Detection and Ranging (LiDAR)
Electronic Warfare (EW) payloads:
- Communication Monitoring and Intelligence (COMINT)
- Radar Emitting Sensing Equipment (RADINT)
- Ground Penetrating Radar (GPR)

Synthetic Aperture Radar (SAR)
Equipped with an Active Electronically Scanned Array (AESA) Synthetic Aperture Radar (SAR) payload, the SKELDAR V-150 provides Ground Moving Target Indicator (GMTI) capabilities and superior imaging enabling high precision ground-mapping and surveillance to take place in all weather conditions. The SAR unit’s low weight enables installation in combination with EO/IR payloads.

Modular and Intuitive RPS Solutions
User friendly and easy to integrate, UMS SKELDAR can provide a full range of Remote Pilot Stations (RPS) including man portable, on and off-road vehicle-mounted and intermodal container systems. Our professional and dedicated team of engineers can integrate an RPS into existing mobile or stationary infrastructure.
Equipment & Serviceability
Technical specification
Performance
Payload:
MTOW:
Data Link Range:
Service Ceiling:
Max. Airspeed:
Fuel:
Endurance:
10 kg in nose (22 lbs)
30 kg in center bay (66.1 lbs)
150 kg (330.7 lbs)
100 km+ (54 NM)
3000 m (9842 ft)
120 km/h (64 kts)
Heavy Fuel (Jet A-1, JP-5 & JP-8)
5 hours*
*Endurance will vary according to payload configuration
Physical
Rotor Diameter:
Airframe Length:
Height:
Width:
3.50 m (11.48 ft)
3.20 m (10.5 ft)
1.00 m (3.28 ft)
0.994 m (3.26 ft)

Skeldar V-150 Unmanned Helicopter in the Media
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