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Alpha Jet

Alpha Jet

Training Jets
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Basic Information
Name
Alpha Jet
Designation
Alpha Jet
Alternate Designation
Alpha Jet A, Alpha Jet ATS, Alpha Jet E, Alpha Jet NGEA
Equipment Type
Training Jets
Manufacturer
Airbus Group, Dassault-Aviation
Date of Introduction
1978
Description

Alpha Jet is a twin-engine, two seats, subsonic trainer developed between France and Germany as a replacement for Magisters and G91s in their respective Air Forces. The French Alpha Jet variant, also known as Alpha Jet E, was intended to provide advanced training for combat aircraft crews. Germany's aircraft were intended for both close air support (CAS) to ground forces and advanced training. German Alpha Jets were designated Alpha Jet A. Both models were powered by two Larzac turbofan engines each rated at 3,175 pounds of thrust. The majority of export aircraft were outfitted like French Alpha Jet E models. The German Alpha Jet A variant features a comprehensive navigation/attack suite and a weapons package including a 27mm or 30mm cannon, bombs, rockets, AIM-9 air-to-air missile and AGM-65 Maverick air-to-surface missile. In the 1980s appeared an improved variant called the Alpha Jet NGEA equipped with new avionics and compatibility with Matra Magic air-to-air missiles. This variant was sold to Egypt and Cameroon. Introduced in the 1990s, Alpha Jet ATS is the latest variant equipped with state-of-the-art avionics, radar and FLIR. In the 1990s Germany retired its Alpha Jet aircraft from service and sold them to Portugal, Greece, UK and Thailand. France continues to operate Alpha Jets but they are expected to be replaced by a new advanced trainer in the upcoming decade.

Air & Air Defense Specifications
Crew 2
Max Speed 957.6 km/h
Range 2600.0 km
Service Ceiling 13000 m
Wingspan 9.10 m
Overview (Deagel)
Group Training Jets
Status Active
Also Known As Alpha Jet A, Alpha Jet ATS, Alpha Jet E, Alpha Jet NGEA
Origin France, Germany
Contractors Airbus Group, Dassault-Aviation
Initial Operational Capability (IOC) 1978
Total Production 500
Specifications (Deagel)
Crew 2
Number of Engines 2
Dimensions — Height 4.2 meter
Dimensions — Length 12.3 meter
Dimensions — Main Gun Caliber 30 millimeter
Dimensions — Wingspan 9.1 meter
Mass — Max Takeoff Thrust 6,350 pound
Mass — Max Takeoff Weight 8,000 kilogram
Mass — Payload 2,200 kilogram
Performance — Ceiling 13,000 meter
Performance — Max Range 2,600 kilometer
Speed — Top Speed at High Altitude 266 mps
Gear (Deagel)
Item 1 Air-to-Air Missiles: AIM-9M Sidewinder
Item 2 Air-to-Air Missiles: R.550 Magic 2
Item 3 Fighter Aircraft Engines: Larzac (2)
Item 4 Standoff Weapons: AGM-65A Maverick
Details
Country of Origin France
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
12.3 m
Width
9.1 m
Height
4.2 m
Weight
8000 kg
Operators (14)
France
Germany
United Kingdom
Belgium
Cameroon
Côte d'Ivoire
Egypt
Greece
Morocco
Nigeria
Portugal
Qatar
Thailand
Togo
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