C-130J Super Hercules



http://www.lockheedmartin.com/content/dam/lockheed/data/aero/documents/global-sustainment/product-support/2012HOC-Presentations/Monday/Mon%201025%20Program%20Brief-John%20Cottam.pdf


Specifications (C-130J)


Specifications are for basic J-model; data for C-130J-30 noted.
Data from USAF C-130 Hercules fact sheet,[75] International Directory of Military Aircraft[76] Encyclopedia of Modern Military Aircraft[3]
General characteristics
Crew: 3 (two pilots, and one loadmaster are minimum crew)
Capacity:
92 passengers (128 for C-130J-30) or
64 airborne troops (92 for C-130J-30) or
6 pallets (8 pallets for C-130J-30) or
74 litter patients with 2 medical personnel (97 litters for C-130J-30)
2–3 Humvees, or 1 LAV III(with turret removed) or an M113 armored personnel carrier
Payload: 42,000 lb (19,050 kg) ; for C-130J-30: 44,000 lb/ 19,958 kg
Length: 97 ft 9 in, 29.79 m (for C-130J-30: 112 ft, 9 in, 34.36 m)
Wingspan: 132 ft 7 in (40.41 m)
Height: 38 ft 10 in (11.84 m)
Wing area: 1,745 ft² (162.1 m²)
Empty weight: 75,562 lb (34,274 kg)
Useful load: 72,000 lb (33,000 kg)
Max. takeoff weight: up to 175,000 lb (79,378 kg); normal 155,000 lb (70,305 kg)
Powerplant: 4 × Rolls-Royce AE 2100D3 turboprop, 4,637 shp (3,458 kW) each
Propellers: Dowty R391 6-blade composite propeller, 1 per engine
Performance
Maximum speed: 362 knots (417 mph, 671 km/h)
Cruise speed: 348 knots (400 mph, 643 km/h)
Range: 2,835 nmi (3,262 mi, 5,250 km)
Service ceiling: 28,000 ft (8,615 m) with 42,000 pounds (19,090 kilograms) payload
Absolute altitude 40,386 ft (12,310 m)[77]
Takeoff distance: 3,127 ft (953 m) at 155,000 lb (70,300 kg) gross weight
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