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De OPLockheed Martin P-3C Orion
Wing: span 99 ft 8 in (30.37 m); aspect ratio 7.5; area 1,300.00 sq ft (120.77 m2)
Fuselage and tail: length 116 ft 10 in (35.61 m); height 33 ft 8.5 in (10.27 m); tailplane span 42 ft 10 in (13.06 m); wheel track 31 ft 2 in (9.50 m); wheel base 29 ft 9 in (9.07 m)
Powerplant: four Allison T56-A-14 each rated at 4,910 ehp (3661 ekW)
Weights: empty 61,491 lb (27890 kg); normal take-off 135,000 lb (61235 kg); maximum take-off 142,000 lb (64410 kg)
Fuel and load: internal fuel 62,500 lb (28350 kg); external fuel none; maximum expendable load 20,000 lb (9072 kg)
Speed: maximum level speed 'clean' at 15,000 ft (4575 m) 411 kt (473 mph;
761 km/h); economical cruising speed at 25,000 ft (7620 m) 328 kt (378 mph; 608 km/h); patrol speed at 1,500 ft (457 m) 206 kt (237 mph; 381 km/h)
Range: operational radius 2,070 nm (2,383 miles; 3835 km) with no time on station or 1,346 nm (1,550 miles; 2494 km) with 3 hours on station
Performance: maximum rate of climb at 1,500 ft (457 m) 1,950 ft (594 m) per minute; service ceiling 28,300 ft (8625 m); take-off run 4,240 ft (1292 m) at maximum take-off weight; take-off distance to 50 ft (15 m) 5,490 ft (1673 m) at maximum take-off weight; landing distance from 50 ft (15 m) 5,490 ft (1673 m) at design landing weight
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[ Bericht 3% gewijzigd door M5 op 20-01-2006 12:28:45 ]