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De OPUS Navy designation: F-14
F-14D
Wing: span 64 ft 1.5 in (19.54 m) spread, 38 ft 2.5 in (11.65 m) swept and 33 ft 3.5 in (10.15 m) overswept: aspect ratio 7.28 ;area 565.00 sq ft (52.49 m)
Fuselage and tail: length 62 ft 8 in (19.10m); height 16 ft 0 in (4-88 m) tailplane span 32 ft 8.5 in (9.97 m); wheel track 16 ft 5 in (5.00 m ); wheel base 23 ft 0 in (7.02 m)
Powerplant: two General Electric F110-GE-400 turbofans each rated at 14,000 lb st (62.27 kN) dry and 23,100 lb st (102.75 kN) with afterburning
Weights: empty 41,780 lb (18951 kg); normal take-off 64,093 lb (29072 kg) for a fighter/escort mission or 73,098 lb (33157 kg) on a fleet air defense mission; maximum take-off 74,349 lb (33724 kg) lb
Speed: maximum at high altitude Mach 1.88 (1,584 mph; 2548 km/h); cruising speed at optimum altitude 413 kt (475 mph;
764 km/h) Range: maximum range with internal and external fuel about 1,600 rmn (1,842 miles; 2965 km); combat radius on a combat air patrol with six AIM-7 Sparrows and four AIM-9 Sidewinders 1,075 nm (1,239 miles; 1994 km)
Performance: maximum rate of climb at sea level more than 30,000 It (9145 m) per minute; service ceiling more than 53,000 ft (16150 m); take-off run 2,500 ft (762 m) from land at maximum take-offweight; landing run 2,400 ft (732 m) on land
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vorige deeltjes
http://ptaslowchat.tk
De code voor de op is hier te vindenChat on
[ Bericht 1% gewijzigd door M5 op 21-01-2006 23:03:00 ]