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Mohajer-1 Iranian Tactical Unmanned Aerial Vehicle (UAV)

Qods Mohajer

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Basic Information
Name
Mohajer-1 Iranian Tactical Unmanned Aerial Vehicle (UAV)
Designation
Qods Mohajer
Alternate Designation
Qods Mohajer; Mohajer-1
Equipment Type
Manufacturer
Qods Aviation
Date of Introduction
1986
Description

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. The Mohajer-1 had a narrow cylindrical fuselage, twin tailbooms, and straight wings mounted high and to the rear of the body. It had a single engine (unknown model) in a pusher configuration, and was guided by ailerons on the wings, an elevator on the horizontal stabilizer, and rudders on the tailbooms. The Mohajer-1 had three fixed landing gear for launch and recovery. It could also be recovered by parachute.The Mohajer-1 was about 8 feet long and had a wingspan of about 10 feet. The Mohajer-1 carried a single still camera, probably carrying photographic film developed after the drone landed. It was controlled by hobby-class radio, which was easily jammed. In addition, Iran attempted to arm it with six RPG-7 rockets, three under each wing, though this was not very successful. This initial variant was used during the later stages of the Iran-Iraq war. It was typically launched from speedboats to provide battlefield surveillance. Unlike later models, the Mohajer-1 featured tricycle landing gear. It had a range of up to 19 mi (30 km) and carried a static nose-mounted camera. The air vehicle could be armed with up to six PG-7 rockets, with three under each wing.

Air & Air Defense Specifications
Endurance 1.50 hrs
Variants
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.[13] 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 Qods Mohajer; Mohajer-1
Type of UAV Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer Qods Aviation, Tehran
Family Mohajer family
In Service 1986-no longer in service
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 INA
Autopilot No
Ceiling, Normal Operations INA km
Endurance 1.5 houors
Range 30 km
Date Transmit Distance INA
Location Positioning System INA
Launch System Runway
Recovery System 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
Note Used during the Iran–Iraq War.
Proliferation Iran, Syria, Venezuela, Hezbollah
Dimensions
Length 2.43 m
Width (Wing Span) 3.04 m
Height INA
Weight, Maximum Takeoff 83 kg
Weight, Payload INA
Tailbooms Twin
Wing Type straight wings mounted high and to the rear of the body
Automotive
Engine Name INA
Engine Type Single Engine
Engine Power INA
Cruising Range 30 km
Speed, Maximum 180 km/h
Speed, Average INA
Endurance 1.5 hours
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
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 No
Still Camera static nose-mounted camera
Thermal Imaging Sensors INA
Electro Optical Pod INA
SAR/GMTI No
SIGINT No
ELINT No
Protection
Fuselage Narrow cylindrical 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 Iran
Category Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Air > Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.43 m
Width
3.04 m
Height
Weight
6.3 kg
Operators (3)
Iran
Syria
Venezuela
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