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Heron
TP MALE UAV Unmanned Aerial Vehicle |
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The
Heron TP MALE also nammed Eitan in Israel, is a variant of Heron Medium
Altitude Long Endurance (MALE) Unmanned Air Vehicle (UAV). Heron TP
is an advanced, multi-purpose MALE UAS with an extended performance
envelope and a variety of payloads capability. The Heron TP was designed
as a multi-purpose, multi-system platform to address local and international
customers' needs and to perform a variety of strategic missions with
a high level of reliability. In April 2004, the Israeli Air Force magazine
announced the existence of the programme and reported that two prototypes
were already flying. In March the following year, US company Aurora
Flight Sciences announced a joint venture to market the aircraft under
the name Orion. Aurora hoped to have a machine flying during 2007, but
by the middle of that year, the company had not released anything further
about the project. Meanwhile reports emerged of a "first flight"
for the Eitan in Israel on 15 July 2006, despite the previous reports
that the aircraft had already been flying two years previously. The
Heron TP was publicly unveiled at a media event at Tel Nof Airbase on
8 October 2007. One report stated that Israel deployed Eitans in its
alleged 2009 airstrike against a Gaza-bound Iranian arms convoy traveling
through Sudan. In February 2010 the Israeli Air Force unveiled its new
fleet of Eitans. The first unit to operate the type, 210 Squadron, was
inaugurated at Tel Nof in December 2010. |
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| Variants |
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| Technical
Data |
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| Design |
| As
medium-altitude, long endurance (MALE) UAV,the HERON TP can
operate at altitudes above commercial air traffic and features
all-weather capability, de-icing systems, automatic takeoff
and landing (ATOL) systems, and triple-redundant avionics. It
is a high-wing cantilever monoplane with wings of high aspect
ratio. Booms extend rearward from the wings and carry twin tails
that are joined by a common horizontal stabiliser. The main
units of the tricycle undercarriage retract into the tail booms,
and the nosewheel retracts into the fuselage. A single turboprop
engine is mounted in the rear fuselage, driving a pusher propeller.
Construction throughout is of composite materials.
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| Mobility |
| The
Heron TP MALE is powered by a turboprop engine developing 1,200-hp
of power. The new engine allows the UAV to achieve an operational
ceiling of 45,000-ft carrying maximum payload which stands above
the commercial aviation traffic. |
| Accessories |
A
data link provides line-of-sight communications while optionally
Satellite Communications (SATCOM) may enable operations beyond
line-of-sight (BLOS). The Heron TP MALE can be equipped with
Electro-Optical (IR/TV) sensors, Synthetic Aperture Radar (SAR),
Electronic Intelligence (ELINT), Communications Intelligence
(COMINT) and Multi-Purpose Radar.
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| Combat
use |
| The
Heron TP MALE can loiter for 36 hours carrying a 1,000 kg sensor
package in its spacious payload compartment. The variety of
sensors can operate simultaneously with multiple configurations.
Heron TP is suitable for all weather conditions and features
autonomic take off and landing (ATOL) with maximum safety, retractable
landing gear, triple fully redundant avionics as well as easy,
safe and reliable operation.
The HERON TP main features and capabilities are:
- Multi mission platform with multiple operational configurations
- Large internal volume for a variety of payloads
- Simultaneous and flexible operation of payloads
- All weather capability
- Operation above commercial traffic
- Satellite communication for extended range (SATCOM)
- Automatic Takeoff and Landing (ATOL) systems for maximal safety
- Triple, fully redundant, state-of-the-art avionics
- Retractable landing gear
- Safe, reliable and easy operation
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| Specifications |
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Type |
| Medium
altitude long endurance Unmanned Aerial Vehicle |
Country
users |
| Israel |
Designer
Country |
| Israel
|
Accessories |
| Electro-optical
sensors, Synthetic Aperture Radar, Communications
Intelligence, Multi-purpose radar |
Operators |
? |
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Engine |
1,200
hp Turbo Engine
a |
Weight |
4,650
kg |
Altitude |
45,000
fts |
Endurance |
36
hr
a
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Dimensions |
Length,
14 m; Wingspan, 26 m |
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