SKELDAR V-150

Supporting Critical Scenarios

SKELDAR V-150

Designed to Deliver Intelligence & Support Tactical Operations

Suitable for deployment in a wide range of operating scenarios, the runway independent Vertical Take-off and Landing (VTOL) SKELDAR V-150 has been designed to support emergency response, tactical surveillance, homeland security and time critical, high-risk search operations. Deployable from non-permissive sites and ideally suited to irregular environments, the SKEDLAR V-150 heightens situational awareness by delivering real-time communications intelligence for extended periods in high-threat scenarios.

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SKELDAR V-150

System Introduction

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).

FULL DATA
V-150 BROCHURE

Slide MAX AIRSPEED DATA RANGE ENDURANCE FUEL PAYLOAD MAX AIRSPEED PAYLOAD FUEL ENDURANCE DATA RANGE

120 km/h

Multiple

120 km/h

Multiple

100 km+

5+ Hours

Heavy Fuel

Heavy Fuel

5+ Hours

100 km+

SKELDAR V-150

Key Features

SKELDAR V-150

Payload Flexibility

Layer
Layer
Layer
Layer
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SKELDAR V-150

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)
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PAYLOAD

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.

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REMOTE PILOT STATION

Modular and Intuitive RPS Solutions

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.

SKELDAR V-150

Equipment & Serviceability

Support Equipment

The SKELDAR V-150 is supplied with all necessary ground support equipment including a ground vaentilator, power unit, generator, refueling system, fire extinguisher, ground-handling wheels, and all required tools.

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Class Leading Serviceability

UMS SKELDAR’s UA’s achieve high Times Between Overhauls (TBO) thanks to superior engine longevity and the use of high-grade components throughout. Routine service procedures can be carried out by technicians in the field without the need for special tools or equipment.

Efficient Ground-Handling

Skid-mounted ground-handling wheels enable efficient pre-deployment maneuverability, preparation, and transportation. Lockable with two pins, ground-handling wheel installation and removal takes seconds and requires minimum effort.

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Engine Servicing & Overhauls

The SKELDAR V-150 introduces the industry’s first and only thirty minute engine removal and replacement system. The engine Line Replacement Unit (LRU) can be exchanged by technicians in the field without the need for special tools or equipment.

SKELDAR V-150

Technical spefications

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)

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SKELDAR V-150

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