|
Fuji T-1 Hatsitaka
 First post-war jet aircraft of Japanese design, the prototype T1F2 flew for the first time on January 19, 1958, powered by a 4,000 lb thrust Bristol Siddeley Orpheus 805 turbo-jet. Two production batches of 20 of this version were built as standard two-seat intermediate jet trainers for the Japanese Air Self-Defence Force, under the designation T1A.
They were followed by the all-Japanese T1F1 (JASDF designation TIB) with a 2,645 lb thrust J3 IHI 3 turbojet produced by Ishikawajima-Harima. The prototype of this version flew on May 17, 1960, and 20 production models were ordered by the JASDF for delivery between August 1962 and March 1963.
 Fuji T1F2 (T1A)
T1A / T1F2
Engine: 1 x 4,000 lbs.t. (1814 kgp) Bristol Siddeley Orpheus 80506.
Span: 34 ft 5.5 in (10.5 m)
Length: 39 ft 9.25 in (12.12 m)
Wing area: 239 sq.ft (22.22 sq.m)
Height: 13ft 3in
Empty weight: 5,335 lb (2 420 kg)
Loaded weight: 9,150 lb (4 238 kg)
Gross weight: 10,6701b
Max speed: 576 mph (921 kph) at 20,000ft (6100 m)
Cruise: 397 mph (640 kph)
Initial climb: 3,460 fpm (17.3 m/sec)
Ceiling: 52,490 ft (16000 m)
Range: 806 mls (1297 km).
Max rate of climb at SL: 6,100 ft/min
T1B / T1F1
Engine: 1 x 2,645 lbs.t. (1200 kgp) J3 IHI 3.
|
