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Lockheed C-130 Hercules
During the 1950s the versatile Lockheed C-130 Hercules was originally designed as an assault transport but was adapted for a variety of missions, including: special operations (low-level and attack), close air support and air interdiction, mid-air space capsule recovery, search and rescue (SAR), aerial refueling of helicopters, weather mapping and reconnaissance, electronic surveillance, fire fighting, aerial spraying, Arctic/Antarctic ice resupply and natural disaster relief missions.
Currently, the Hercules primarily performs the intratheater portion of the tactical airlift mission. This medium-range aircraft is capable of operating from rough, dirt strips and is the prime transport for paratroop and equipment drops into hostile areas.
Primary Role: Intratheater tactical airlift Wingspan: 132 feet, 7 inches (40.4m) Length: 97 feet, 9 inches (29.7m) Height at Tail: 38 feet, 3 inches (11.6m) Engines: Four Allison T56-A-15 turboprops Horsepower: 4,300 shp per engine Cruise Speed: 374 mph (602km/h; Mach 0.5) Range: 2,047 nm (3,791km) with max payload; 4,522 nm (8,375km) empty Service Ceiling: 33,000 feet (10,058m) Operating Weight: 83,000 pounds (37,648kg) Fuel Capacity: 60,000 pounds (27,216kg) Max Payload: 45,000 pounds (20,412kg) Max Takeoff Weight: 155,000 pounds (70,307kg) Basic Crew: Five (pilot, co-pilot, navigator, flight engineer, loadmaster) Date Deployed: April 1955