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Panghyon-2 North Korean Unmanned Aerial Vehicle (UAV)

Panghyon-2

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Panghyon-2 North Korean Unmanned Aerial Vehicle (UAV)
Designation
Panghyon-2
Alternate Designation
Panghyon-2
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Date of Introduction
1995
Description

This North Korean variant is based on the ASN-105. It is capable of carrying a combat load of 44 to 55 lb (20 to 25 kg) and reaching an altitude of nearly 9,900 ft (3,000 m). The ASN-105 is a medium tactical unmanned aerial vehicle (UAV) in service with the Chinese People's Liberation Army. It is designed to perform real-time battlefield surveillance and intelligence collection. Guided by GPS navigation, the ASN-105B is launched by rocket boost and lands with a parachute. An ASN-105 system is made up of six UAVs, a main ground-control station, a mobile ground-control station, an image-processing shelter, a TV/infrared image interpreting shelter and a launcher. The ASN-105B may have a redesigned fuselage and changes to the engine. Models displayed in 2004 had a more square-shaped fuselage, increased wing chord and modified engine exhaust. It has a maximum takeoff weight of 350 lb (160 kg) and a ceiling of 19,700 ft (6,000 m). Status The ASN-105A was first delivered to the PLA in the mid-1990s; the ASN-105B is also in service with China. The ASN-105A also serves with Pakistan.

Air & Air Defense Specifications
Engine 1 x HS-510 4-cyl, air-cooled piston (30 hp)
Max Speed 250.0 km/h
Cruise Speed 150.0 km/h
Endurance 2.00 hrs
Wingspan 4.30 m
Variants
ASN 105 ASN-105 is a fixed wing UAV in conventional layout with high wing configuration, and propulsion is provided by a two-blade fixed pitch propeller driven two-stroke engine mounted in the nose. ASN-105 is a development of ASN-104, and thus having identical layout. The main improvement of ASN-105 over its predecessor ASN-104 is that its remote control range is increased by two third, from the original 60 km to 100 km. Another improvement of ASN-105 over its predecessor ASN-104 is that its ground control station is fully computerized.
System
Alternate Designation Panghyon-2
Type UAV
Dimensions
Length 3.32 m
Height .9 m
Wingspan 4.30 m
Wing Area 1.85 sq m
Takeoff Weight 140 kg
Payload 25 kg
Automotive
Engine Name INA
Engine Type 1 x HS-510 4-cyl, air-cooled piston
Engine Power 30 hp
Maximum Speed 250 km/h
Cruise Speed 150 km/h
Maximum Altitude 3,000 m
Endurance 2 hours
Remote Control Maximum Distance 100 km
Armament
Note None
Protection
Note None
Details
Country of Origin North Korea
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
P
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
3.32 m
Width
Height
0.9 m
Weight
140 kg
Operators (1)
North Korea
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