[PTA SC] Lockheed Martin F-16 Fighting Falcon @ 795 kts

De OP
LOCKHEED MARTIN (GENERAL DYNAMICS) F-16 FIGHTING FALCON

F-16 Wing: span 31 ft 0 in (9.45 m) without tip-mounted AAMs and 32 ft 9.75 in (10.00 m) with tip-mounted AAMs; aspect ratio 3.09; area 300.00 sq ft (28.87m2) Fuselage and tait length 49 ft 4 in (15.03 in); height 16 ft 8.5 in J5.09 m); tailplane span 18 ft 3.75 in J5.58 m); wheel track 7 ft 9 in (2.36 m); wheel base 13 It 1.5 in J4.00 m) Powerplant (see text for sub-variant) one Pratt & Whitney FlOO-P-220 turbotan rated at 23,450 lb st 1104.31 kN) with afterburning or one General Electric FIIO-GE-100 turbofan rated at 27,600 lb st (122.77 kN) with afterburning Weights: empty 19,100 lb (8663 kg) with F110turbofan or 18,335 lb (8316 kg) with F100 turbofan; typical combat take-off 21,585 lb (9791 kg); maximum take-off 25,071 lb (11372 kg) for an air-to-air mission without drop tanks or 42,300 lb (19187 kg) with maximum external load Fuel and load: internal fuel 6,972 lb (3162 kg); external fuel up to 6,760 lb (3066 kg) in three 300-, 370-, 450- and 600-US gal (1136, 1400-,1703- and 2271 -litrel drop tanks; maximum ordnance 15,200 lb J6894 kq) Speed: maximum level speed 'clean' at 40,000 It (12190 m) more than 1,146 kt (1,320 mph; 2124 km/h) and at sea level 795 kt (915 mph; 1472 km/h) Range: ferry range more than 2,100 nm (2,418 miles; 3891 km) with drop tanks; combat radius 295 nm (340 miles; 547 km) on a hi-lo-hi mission with six 454 kg (1,000 lb) bombs Performance: maximum rate of climb at sea level more than 50,000 ft (15240 m) per minute; service ceiling more than 50,000 ft (15420 m) g limits: +9







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Chat on

meer pics volgen nog

quote:

Op maandag 6 februari 2006 16:37 schreef hermandeperman het volgende:
Weer een vliegtuig?

Dan ga ik nu deze pagina eens even flink verzieken met bootjes foto's !

[afbeelding]

berge stahl