Overview
The Panavia Tornado IDS was developed as a multinational strike aircraft for high-speed, low-level missions in contested airspace. Built through cooperation between the United Kingdom, Germany, and Italy, it became one of NATO’s principal strike platforms during the Cold War. The IDS variant formed the backbone of the Tornado fleet.
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Specifications
Units
- Engine
- 2 × Turbo-Union RB199-34R Mk 103
- Engine type
- Turbofan
- Thrust
- 2 × 17,300 lbf · 77 kN
- Avionics
- Rafael LITENING, GEC Sky Shadow
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 54 ft 10 in · 16.72 m
- Tail height
- 19 ft 6 in · 5.95 m
- Fuselage diameter
- —
- Wing span
- 45 ft 8 in · 13.91 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 61,500 lb · 28,000 kg
- Max landing weight
- —
- Max payload
- 19,800 lb · 9,000 kg
- Fuel capacity
- 1,230 gal · 4,700 L · 3,700 kg (Jet A)
- Max cruise speed
- 1,313 kt · 1,511 mph · 2,432 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 750 nm · 860 mi · 1,390 km
- Fuel burn
- 1.00 nm/gal · 0.49 km/L
- Ceiling
- 50,000 ft · 15,200 m
- Rate of climb
- 15,100 ft/min · 77 m/s
- Takeoff distance
- 2,500 ft · 760 m
- Landing distance
- 1,210 ft · 370 m
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