Lockheed C-130 Hercules

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The Lockheed C-130 Hercules is an American four-engine turboprop military transport aircraft designed and built originally by Lockheed (now Lockheed Martin). Capable of using unprepared runways for takeoffs and landings, the C-130 was originally designed as a troop, medevac, and cargo transport aircraft. The versatile airframe has found uses in a variety of other roles, including as a gunship (AC-130), for airborne assault, search and rescue, scientific research support, weather reconnaissance, aerial refueling, maritime patrol, and aerial firefighting. It is now the main tactical airlifter for many military forces worldwide. More than 40 variants of the Hercules, including civilian versions marketed as the Lockheed L-100, operate in more than 60 nations.

The C-130 entered service with the U.S. in 1956, followed by Australia and many other nations. During its years of service, the Hercules family has participated in numerous military, civilian and humanitarian aid operations. In 2007, the C-130 became the fifth aircraft[N 1] to mark 50 years of continuous service with its original primary customer, which for the C-130 is the United States Air Force. The C-130 Hercules is the longest continuously produced military aircraft at over 60 years, with the updated Lockheed Martin C-130J Super Hercules currently being produced.

General characteristics

  • Crew: 5 (2 pilots, CSO/navigator, flight engineer and loadmaster)
  • Capacity: 42,000 lb (19,000 kg) payload
    • C-130E/H/J cargo hold: length, 40 ft (12.19 m); width, 119 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 in (3.12 m); width, 119 in (3.02 m)
    • C-130J-30 cargo hold: length, 55 ft (16.76 m); width, 119 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 inches (3.12 m); width, 119 in (3.02 m)
    • 92 passengers or
    • 64 airborne troops or
    • 74 litter patients with 5 medical crew or
    • 6 pallets or
    • 2–3 Humvees or
    • 2 M113 armored personnel carriers
    • 1 CAESAR self-propelled howitzer
  • Length: 97 ft 9 in (29.79 m)
  • Wingspan: 132 ft 7 in (40.41 m)
  • Height: 38 ft 3 in (11.66 m)
  • Wing area: 1,745 sq ft (162.1 m2)
  • Airfoil: root: NACA 64A318; tip: NACA 64A412
  • Empty weight: 75,800 lb (34,382 kg)
  • Max takeoff weight: 155,000 lb (70,307 kg)
  • Powerplant: 4 × Allison T56-A-15 turboprop engines, 4,590 shp (3,420 kW) each
  • Propellers: 4-bladed Hamilton Standard 54H60 constant-speed fully feathering reversible propellers, 13 ft 6 in (4.11 m) diameter 

Performance

  • Maximum speed: 320 kn (370 mph, 590 km/h) at 20,000 ft (6,100 m)
  • Cruise speed: 292 kn (336 mph, 541 km/h)
  • Range: 2,050 nmi (2,360 mi, 3,800 km)
  • Service ceiling: 33,000 ft (10,000 m) empty
23,000 ft (7,000 m) with 42,000 lb (19,000 kg) payload
  • Rate of climb: 1,830 ft/min (9.3 m/s)
  • Takeoff distance: 3,586 ft (1,093 m) at 155,000 lb (70,307 kg) max gross weight;
1,400 ft (427 m) at 80,000 lb (36,287 kg) gross weight

Avionics


copied by wikipedia.

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