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Harop Israeli Loitering Munition Unmanned Aerial Vehicle (UAV)

Harop

Loitering Munition UAV
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Basic Information
Name
Harop Israeli Loitering Munition Unmanned Aerial Vehicle (UAV)
Designation
Harop
Alternate Designation
Harop; Harpy 2
Equipment Type
Loitering Munition UAV
Manufacturer
Israel Aerospace Industries (IAI)
Date of Introduction
2009
Description

The HAROP is a standoff loitering attack weapon system designed to locate and precisely attack targets. The HAROP loitering missile (LM) type platform serves as an Electro-Optically guided attack weapon. HAROP LMs are launched from ground-based launchers and controlled via a two-way data link for full man-in-the-loop operation. HAROP is used to attack high-value targets, including full mission capabilities, from search, through the attack, and up to battle damage assessment. Combining characteristics of a missile and a UAV, HAROP enables effective mission execution without relying on other external systems for targeting and mission intelligence The HAROP LMs are programmed before launch by the GCS to autonomously fly to a pre-defined “Holding Area”, where they loiter. The MCS periodically checks their position and status during the route to the “Holding Area”. The MCS operator can thus control a number of HAROP LMs that loiter over a “Holding Area”, he can select one LM for target search and attack, while the others are monitored periodically. The operator directs the selected LM to the target area and uses the video image to select a target and to attack it. The HAROP tracks the target and then dives on it, detonating the warhead upon impact. If required the attack can be aborted and the operator can re-attack with the same LM.

Air & Air Defense Specifications
Engine Rotary Engine (38 hp)
Max Speed 416.7 km/h
Endurance 9.00 hrs
Wingspan 3.00 m
System
Alternative Designation Harop; Harpy 2
Type Loitering Munition Unmanned Aerial Vehicle (UAV)
Manufacturer Israel Aerospace Industries (IAI)
Ground Crew 3-4 (Est)
Flight Control Mission Control Shelter (MCS) controls vehicle with a “man-in-the-loop” able to engage or abort the attack in real time. In event of an abort, reverts to loiter mode until attack is restarted.
Launch Method Solid-propellant booster rocket from ground-based storage container
Recovery / Landing Method Intentionally expendable, non-recoverable
Launcher Trucks per Battery INA
Missiles per Launcher 12 ea
Total Missiles per Battery INA
Precision Strike Less than 1 meter precision strike with 16 Kg warhead
Dimensions
Length, Overall 2.5 m
Height, Overall 0.3 m
Wingspan 3.0 m
Weight, Maximum Launch 135 kg
Automotive
Engine Name INA
Engine Type Rotary Engine
Engine Power 38 hp
Propulsion Rotary engine driving a 2-blade pusher propeller
Maximum Speed 416.7 km/h
Range 1,000 km
Communication Range 200 km
Endurance up to 9 hours
Maximum Altitude 4,572 m
Payload
Passive Rada Seeker Sensor Wide range of frequencies
Electro Optical Color CCD, FLIR (IAI Tamam POF-200)
User Image Capabilities Images recieved via satcom datalink.
Missile HE-Frag warhead
Max Payload with Warhead 23 kg
Note The Harop missiles can be launched from various transportable platforms including sea and ground based canisters or air launched to navigate towards the potential target area. It can be launched at any angle, at a horizontal or vertical trajectory. The sealed container ensures it copes with harsh battlefield conditions. The launcher has a fuelling system to provide all-time readiness.
Details
Country of Origin Israel
Category UAVs
Air > UAVs
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.5 m
Width
Height
0.3 m
Weight
135 kg
Operators (6)
Germany
Israel
Turkey
India
Azerbaijan
Singapore
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