Overview
The Dornier Alpha Jet is a twin-engine jet trainer and light attack aircraft developed jointly by Germany and France. Designed for both pilot training and close air support, it entered service in the 1970s. The aircraft became a standard advanced trainer in several air forces.
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Specifications
Units
- Engine
- 2 × SNECMA Turbomeca Larzac 04-C6
- Engine type
- Turbofan
- Thrust
- 2 × 3,000 lbf · 13 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 43 ft 5 in · 13.23 m
- Tail height
- 13 ft 9 in · 4.19 m
- Fuselage diameter
- —
- Wing span
- 29 ft 11 in · 9.11 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 17,600 lb · 8,000 kg
- Max landing weight
- —
- Max payload
- 5,500 lb · 2,500 kg
- Fuel capacity
- 500 gal · 1,900 L · 1,500 kg (Jet A)
- Max cruise speed
- 540 kt · 621 mph · 1,000 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 90 kt · 104 mph · 167 km/h
- Range
- 1,590 nm · 1,830 mi · 2,940 km
- Fuel burn
- 3.43 nm/gal · 1.68 km/L
- Ceiling
- 50,000 ft · 15,200 m
- Rate of climb
- 12,000 ft/min · 61 m/s
- Takeoff distance
- 1,350 ft · 410 m
- Landing distance
- 2,000 ft · 610 m
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