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Heron TP (Eitan) Israeli Unmanned Aerial Vehicle (UAV)

Heron TP

Multirole Fighter Aircraft
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Basic Information
Name
Heron TP (Eitan) Israeli Unmanned Aerial Vehicle (UAV)
Designation
Heron TP
Alternate Designation
Heron TP; Eitan
Equipment Type
Multirole Fighter Aircraft
Manufacturer
Israel Aerospace Industries (IAI)
Date of Introduction
2018
Description

The Heron TP is a multi-role, advanced, long-range Medium Altitude Long Endurance (MALE) Unmanned Aerial System (UAS) for strategic missions. It is equipped with automatic taxi-takeoff and landing systems (ATOL), satellite communication (SATCOM) for extended range, fully redundant avionics, and more. The Heron TP was designed as a multi-mission platform to address local and international customers' needs and to perform a variety of strategic missions, including intelligence gathering, surveillance, target acquisition, and reconnaissance, using various payloads, with a high level of reliability.

Air & Air Defense Specifications
Engine Turboprop (1200 hp)
Max Speed 407.4 km/h
Range 1000.0 km
Endurance 30.00 hrs
Wingspan 26.00 m
Variants
Heron (Machatz-1) The IAI Heron (Machatz-1) is a medium-altitude long-endurance unmanned aerial vehicle (UAV) developed by the Malat (UAV) division of Israel Aerospace Industries. It is capable of Medium Altitude Long Endurance (MALE) operations of up to 52 hours' duration at up to 10.5 km (35,000 ft). It has demonstrated 52 hours of continuous flight, but the effective operational maximal flight duration is less, according to payload and flight profile. An advanced version, the Heron TP, is also known as the IAI Eitan.
System
Alternate Designation Heron TP; Eitan
Type Medium-Altitude, Long-Endurance (MALE) Unmanned Aerial Vehicle (UAV)
Manufacturer Israel Aerospace Industries.
Crew Unmanned
Maximum Payload Capacity 2,700 kg
Electro Optical Payload M-19 HD Electro Optical Payload (TV & IR Combi or Multi Sensor TV/IR/LRF/LD) , WIDEEYE Scan
Radar Synthetic Aperture Radar (SAR)
Communications Communications Intelligence (COMINT - HF, VHF, UHF/ DF)
Avionics Triple redundant avionics
Configuration Multi mission/multi payload configurations
Global System Mobile (GSM) Yes
Electronic Support Measures /Electronic intelligence (ESM/ELINT) Yes
Maritime Patrol Radar (MPR) Yes
Identification, Friend or Foe (IFF) Yes
Traffic collision avoidance system (TCAS) Yes
Integrated ATC Communication Relay Yes
Direct Line-of-Sight (LOS) data link Yes
Satellite Communication (SATCOM) Yes
UAV airborne data relay (ADR) for beyond LOS missions Yes
Ground-based data relay (GDR) for beyond LOS missions Yes
Taki-Takeoff Automatic Taxi-takeoff and Landing (ATOL)
All Weather Capability Yes
Dimensions
Length 14 m
Wingspan 26 m
Height INA
Maximum Take-Off Weight 5,670 kg
Automotive
Engine Name 2 x PT6
Engine Type Turboprop
Engine Power 1,200 hp
Maximum Speed 407.44 km/h
Range 1,000 km
Maximum Altitude 13,716 m
Endurance 30 hours
Details
Country of Origin Israel
Category UAVs
Air > UAVs
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
14 m
Width
26 m
Height
Weight
5670 kg
Operators (2)
Israel
India
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