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Arpia Venezuela Tactical Unmanned Aerial Vehicle (UAV)

CAVIM Arpia, Arpia

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Basic Information
Name
Arpia Venezuela Tactical Unmanned Aerial Vehicle (UAV)
Designation
CAVIM Arpia, Arpia
Alternate Designation
CAVIM Arpia, Arpia
Equipment Type
Manufacturer
Qods Aviation
Date of Introduction
2009
Description

In 2007, Venezuela signed an agreement with Iran to assemble 12 Mohajer-2 UAVs from knock-down kits supplied by Quds. Venezuelan state-owned defense contractor CAVIM began assembling the drones by 2009. US satellite imagery revealed the facility manufacturing the drones in 2010, and they were unveiled to the public as the CAVIM Arpia in 2012.

Air & Air Defense Specifications
Endurance 90.00 hrs
Variants
Mohajer-1 The Mohajer was Iran's first drone to enter series production and was used during the Iran–Iraq War. The Mohajer-1 was known simply as "Mohajer" through the 80s and 90s, when it was re-designated "Mohajer-1" as other Mohajer variants had been developed.
Mohajer-2 Following the successful use of the Mohajer-1, Iran wanted a version with more range and endurance. This version, which would later be named the Mohajer-2, also had an auto pilot system to fly beyond the line-of-control of its command center.
Mohajer-2N In 2014, Iran introduced the Mohajer-2N, which shares the same design as the Mohajer-2 but has far improved performance. The Mohajer-2N replaces the electronics of the Mohajer-2 with more modern versions and has also has improved flight characteristics. T
Mohajer-3 The Mohajer-3, also known as the Dorna, was designed with a new airframe for better performance. It had a square body and featured a low-mounted horizontal stabilizer flush with the main wing, the only member of the Mohajer family configured this way.
Mohajer-4 The Mohajer-4 was designed for both the Iranian Army and the IRGC and entered service in late 1997.
Mohajer-4B Also known as the Sadiq, the Mohajer-4B is a significant evolution of the Mohajer-4 platform with a square fuselage, twin tail booms, a top-mounted horizontal stabilizer, uncanted wingtips, new landing skids, and straight wings mounted high and to the mid of the body
Sadegh-1 The Sadegh-1 ("Honest-1"), also known as the QOM-1, is simply a Mohajer-4B with two MANPADS mounted on pylons.It was tested in late 2014
Mohajer-6 The Qods Mohajer-6 is a persistent ISTAR UAV capable of carrying a multispectral surveillance payload and/or up to two precision-guided munitions. Ten have been manufactured as of February 2018 for the IRGC Ground Forces, and 40 are planned for the IRGC Navy.The Mohajer-6 complements the larger Shahed 129 operated by the third IRGC branch, the IRGC-ASF. Three have also been delivered to the Iranian Army.
System
Alternative Designation CAVIM Arpia, Arpia
Type of UAV Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer Qods Aviation, Tehran
Family Mohajer family
In Service 2009-Present
Flight Control Method controlled by hobby-class radio, which was easily jammed
Day/Night Capable INA
All Weather Capable INA
Takeoff or Landing Limitations INA
Ground Crew Capable of being controlled via land crew or autopilot
Autopilot Yes, which controls the aircraft via waypoints
Endurance 90 min
Range 30 km
Date Transmit Distance INA
Location Positioning System Yes
Launch System PL3 pneumatic catapult
Recovery System Skid Landing or Parachute
Number of Hard Points 6 ea
Manned-Unmanned Teaming (MUM-T) Capable No
Automatic Landing and Takeoff Capability No
Landing Gear three fixed landing gear for launch and recovery
Stabilizer Horizontal stabilizer
Antenna Type two stub antenna in the under 10 GHz range, one on each wing, for real-time control.
Note #1 Designed for surveillance use
Note #2 the Arpia lacks over-the-horizon guidance
Proliferation Valenzuela
Dimensions
Length 2.9 m
Width (Wing Span) 3.8 m
Height INA
Weight, Maximum Takeoff 83 kg
Weight, Empty 70 kg
Tailbooms Twin
Wing Type Mid-mounted, untapered wings
Tail Type Horizontal tail
Automotive
Engine Name WAE-342 Engine
Engine Type Single Engine
Engine Power 25 hp
Cruising Range 30 km
Speed, Maximum 200 km/h
Speed, Average INA
Endurance 90 min
Maximum Ceiling 4,820 m
Radius 50 km
Cargo Capacity (Payload) 15 kg
Propellers 2-bladed
Rudders Twin Rudders
Belly Skid Yes, The belly skids are non-retractable, but can compress on landing to reduce shock
Communications
Radio INA
Retrans Radio INA
Main Weapons System
Name RPG-7
Type Rocket-propelled grenade launcher[
In Service 1961-Present
Manufacturer Bazalt and Degtyarev plant (Russian Federation)
Proliferation + 9 Million
Length 950 mm
Cartridge 85 mm
Caliber 40 mm
Weight 6.3 kg
Muzzle Velocity, Boost 115 m/s
Muzzle Velocity, Flight 300 m/s
Effective Firing Range 300 m
Maximum Firing Range 700 m (OG-7V) (self detonates at ≈920 m (1,000 yd))
Sights PGO-7 (2.7×), UP-7V Telescopic sight and 1PN51/1PN58 night vision sights Red dot reflex sight
Basic Load 12 ea
Fire Control
Fire Control System Type INA
Fire Control Radar No
Radar Type INA
Radar Designator INA
Laser Rangefinder INA
Laser Designator INA
Full-Motion Video Yes, video and infrared with 1-m resolution mounted on the forward part of the fuselage
Still Camera static nose-mounted camera
Thermal Imaging Sensors No infrared camera installed
Electro Optical Pod INA
Forward-Looking Infrared (FLIR) Sensors. Yes
Onboard Digital Processor Yes, which can downlink sensor imagery
Navigation Camera fixed forwards-facing camera for navigation
Guidance System GPS Guidance System
Note A line-scanner is provided, which reportedly can provide 3-ft (1-m) resolution at an altitude of 16,400 ft (5,000 m)
Protection
Fuselage Bullet-shaped fuselage
Stealth Properties No
Heat Signature Reduction No
Add on Armor No
EW No
EW Counter Measures / CCM No
Counter Measures (Chaffs/Flares) No
Details
Country of Origin Venezuela
Category UAVs
Air > UAVs
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.9 m
Width
3.8 m
Height
Weight
6.3 kg
Operators (1)
South America
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