Fuji T-1
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The Fuji T-1 was Japan's first jet-powered trainer aircraft. The first flight was in January 1958.It's retired March 2006.
Variants
- T1F1 : Prototype.
- T-1A : The T-1A is powered by a 1814-kg (4,000-lb) Rolls-Royce Orpheus Mk 805 turbojet engine. The original designation was T1F2.
- T-1B : The T-1B is powered by a 1200-kg (2,646-lb) Ishikawajima-Harima IHI J3-IHI-7B turbojet engine.
- T1F3 : Prototype.
- T-1C :
Specifications (T-1A)
General characteristics
- Crew: two, student and instructor
- Length: 12.12 m (39 ft 9 in)
- Wingspan: 10.49 m (34 ft 5 in)
- Height: 4.08 m (13 ft 4 in)
- Wing area: m² ( ft²)
- Empty: 2,420 kg (5,335 lb)
- Loaded: kg ( lb)
- Maximum takeoff: 5,000 kg (11,023 lb)
- Powerplant: 1 × Rolls-Royce Orpheus Mk 805, 17.8 kN (4,000 lbf) thrust
Performance
- Maximum speed: 920 km/h (575 mph)
- Range: 1,850 km (1,156 miles)
- Service ceiling: 14,400 m (47,250 ft)
- Rate of climb: m/min ( ft/min)
- Wing loading: kg/m² ( lb/ft²)
- Power/Mass: kW/kg ( hp/lb)
Armament
- None (In war time,1 × 12.7 mm Browning M53-2 machine gun)
- up to 680 kg (1,500 lb) of disposable stores.
Operators
Related content
Related development:Comparable aircraft: F-86 Sabre
Designation sequence: T-1 - T-2 - T-3 - T-4
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