Gulfstream Peregrine 600
The Gulfstream American Peregrine 600 was a military trainer aircraft developed in the United States in the early 1980s but which did not progress further than prototype stage. Developed from the company's Hustler business aircraft, the Peregrine shared the same wings, empennage and rear fuselage, but had a new forward fuselage with side-by-side seating for the pilot and instructor. The aircraft was developed as a contender in the United States Air Force's Next Generation Trainer programme, but was ultimately passed over in favour of the Fairchild T-46. Attempts to market it to (at least) the air forces of Australia, New Zealand, Japan, and China also proved unsuccessful, and the project was cancelled in 1985. The wing and rear fuselage design was incorporated in the Gulfstream Aerospace Peregrine business aircraft.
Other articles related to "gulfstream peregrine 600":
... General characteristics Crew 2 Length 38 ft 4 in (11.68 m) Wingspan 34 ft 5 in (10.5 m) Height 13 ft 5 in (4.09 m) Gross weight 5,254 lb (2,383 kg) Max takeoff weight 6,199 lb (2,812 kg) Normal landing weight 4,402 lb (1,997 kg) Powerplant 1 × Pratt Whitney Canada JT15D-4 turbofan engine, 2,500 lbf (11.12 kN) thrust Performance Maximum speed 394 kn (453 mph 730 km/h) at 20,000 ft (6,096 m) Stall speed 66 kn (76 mph 122 km/h) power off Range 1,080 nmi (1,243 mi 2,000 km) at 40,000 ft (12,192 m) and 369 kn (425 mph 683 km/h) Service ceiling 48,000 ft (15,000 m) Rate of climb 5,200 ft/min (26 m/s) at sea level Take-off run to 50 ft (15 m) 489 ft (149 m) Landing from 50 ft (15 m) 639 ft (195 m) at Normal landing weight. ...