Friday, November 14, 2014

C-130J Super Hercules

C-130J Super Hercules (Military transport) – 177


Manufacturer: Lockheed Martin
First flight: 5 April 1996
Introduction: 1999
Produced: 1996-present
Number built: 300 as of 18 December 2013
Unit cost: $67.3 million (flyaway cost, USAF, FY2014)
Developed from: Lockheed C-130 Hercules


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: 19,050 kg (for C-130J-30 – 19,958 kg)
Length: 29.79 m (for C-130J-30 – 34.36 m)
Wingspan: 40.41 m
Height: 11.84 m
Wing area: 162.1 m²


Empty weight: 34,274 kg
Useful load: 33,000 kg
Max. takeoff weight: 79,378 kg; normal: 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


Maximum speed: 671 km/h
Cruise speed: 643 km/h
Range: 5,250 km
Service ceiling: 8,615 m with 19,090 kg payload
Absolute altitude: 12,310 m
Takeoff distance: 953 m at 70,300 kg gross weight

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