SKELDAR V-200

Trusted by Naval Forces Worldwide

For UMS SKELDAR, the ultimate measure of success is knowing that our multiple use Unmanned Aircraft Systems (UAS) support some of the most challenging tactical maritime and overland scenarios for our customers.

Testament to the V-200’s capabilities is the fact that it is the platform of choice for multiple NATO naval forces thanks to its superior intelligence-gathering capabilities and performance.

SKELDAR V-200

Supporting Critical Scenarios

SKELDAR V-200

System Introduction

Rugged components designed to operate in adverse weather and harsh saltwater conditions, ship-based Automatic Take-off, and Landing (ATOL), ship-specific Remote Pilot Station (RPS) integration options, multiple payloads carrying capability and a dependable heavy fuel engine are just some of the features to make the V-200 the ultimate NATO-aligned rotary platform.

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

140 km/h

Multiple

140 km/h

Multiple

100 km+

6+ Hours

Heavy Fuel

Heavy Fuel

6+ Hours

100 km+

V-200 BROCHURE
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SKELDAR V-200

Key Features

SKELDAR V-200

Payload Flexibility

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SKELDAR V-200

Payload Options

As an agnostic platform, the V-200 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

EW and Radar Sensing Payload Benefits

Today’s Unmanned Aircraft Systems (UAS) operate in a complex and multifaceted signals environment. Equipping the V-200 with EW or Radar Emitting Sensing payloads enables the interception, locating, detection, disruption and jamming of signals from potential threats. Situational awareness is heightened and response times from air, sea or land-based forces are reduced.

PAYLOAD

Synthetic Aperture Radar (SAR)

Featuring an under-belly mounted steerable beam antenna and a high-performance Ground Moving Target Indicator (GMTI), Active Electronically Scanned Array (AESA) Synthetic Aperture Radar (SAR) provides reliable high-resolution all-weather day or night intelligence gathering, ground mapping and surveillance capabilities. High reliability and operational availability are achieved by using numerous solid states Transmit/ Receive Modules within a fixed array. The system’s low power consumption, low weight and compact size make SAR installations in combination with Electro-Optical/Infra-Red (EO/IR) sensors and other payloads possible.

Key SAR features:

  • Moving Target Indicator (MTI)
  • Wide Area Coverage
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SKELDAR V-200

Connectivity, Control
& Integration

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SKELDAR V-200

Modular and Intuitive
RPS Solutions

Our Remote Pilot Station (RPS) has been designed to reduce fatigue by providing the highest level of operator comfort. An ergonomic design and an intuitive operator terminal provide excellent mission situational awareness, operational efficiency, and the highest levels of flight safety.

Alongside an extensive range of vehicle-mounted and land-based RPS options, ship-specific RPS integration options are offered, making the V-200 the perfect platform for ship-based operations. UMS Skeldar can facilitate RPS integrations into existing specific operational infrastructure (e.g. vehicles, ships).

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SKELDAR V-200

Technical spefications

Performance

Payload:

MTOW:

Data Link Range:

Service Ceiling:

Max. Airspeed:

Fuel:

Endurance:

Multiple 40 kg (88 lbs)

245 kg (540 lbs)

100 km+ (54 NM)

3000 m (9842 ft)

140 km/h (75 kts)

Heavy Fuel (Jet A-1, JP-5 & JP-8)

6+ hours*
*Endurance will vary according to payload configuration

Physical

Rotor Diameter:

Airframe Length:

Height:

Width:

4.60 m (15 ft)

4 m (13 ft)

1.3 m (4.2 ft)

1.2 m (4 ft)

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SKELDAR V-200

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