Eurocopter Tiger

A
join-venture of Aerospatiale and MBB projected at the end of the 70s and
started in 1984 to provide an attack helicopter to the German ( PAH-2 anti
tank variant ) and French Armies ( HAP / HAC escort variant )
Due highly costs, the program was cancelled in 1986 but was re-launched
during 1987 and 5 prototypes were built.
In the 90s, the demise of the Warsaw Pact threat, forced to Eurocopter
look for the international market.
First flight of the
aircraft was in 1991. Serial production began in March 2002 and the first
flight of the production Tiger HAP for France took place in March 2003.
France has ordered 80 aircraft (70 combat support HAP and 10 antitank HAC
) with deliveries to commence in September 2003.
Germany has ordered 80 UHT combat support aircraft with deliveries to
begin by the end of 2003.
Total procurement is planned to be 120 for France and 120 for Germany.
In December 2001, Eurocopter, with the Tiger ARH (armed reconnaissance),
was awarded the contract for the Australian Army’s Air 87 requirement for
22 helicopters. The Tiger ARH is a modified version of the Tiger HAP with
upgraded MTR390 engines and a laser designator incorporated in the Strix
sight for the firing of Hellfire II air-to-ground missiles. The first
Tiger ARH is scheduled to enter service in 2004. Australian Aerospace (a
subsidiary of Eurocopter) is to set up a local production facility for
assembly of the helicopters and the manufacture of parts for the entire
programme. ADI Ltd will be a major subcontractor, responsible for
customising the mission and communications systems.
In September 2003, Spain selected a version of the Tiger HAP combat
support helicopter to be called the HAD which will be armed with the
Trigat LR and Mistral missile systems. 24 helicopters will be ordered
which will also have an uprated Enhanced MTR390 engine and a heavier
payload. Deliveries are scheduled for 2007-08.


Pilot Crewstation (Front) |

Gunner Crewstation (Rear) |


First Flight :
March 27, 1991
Crew: 2
Type: Attack
Engines: 2 * 1280 shp MTU/Rolls-Royce/Turbomeca MTR390 turbine
engines
Speed : 260 km/h
Rate of climb: 600 m/min
Endurance: 2 h 50 min
Weight: 3300 kg -- Max: 6000
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