MC-130E/H COMBAT TALON I/II
|
|
 |
|
| Fact Sheet Tools |
|
|
|
|
Mission
The MC-130E Combat Talon I and MC-130H Combat Talon II provide infiltration, exfiltration and resupply of special operations forces and equipment in hostile or denied territory. Secondary missions include psychological operations and helicopter air refueling
Features
Both aircraft feature terrain-following and terrain-avoidance radars capable of operations as low as 250 feet in adverse weather conditions. Structural changes to a basic C-130 include the addition of an in-flight refueling receptacle, and strengthening of the tail to allow high speed/low-signature airdrop. Their navigation suites include dual ring-laser gyros, mission computers and integrated global positioning system. They can locate, and either land or airdrop on small, unmarked zones with pinpoint accuracy day or night.
An extensive electronic warfare suite enables the aircrew to detect and avoid potential threats. If engaged, the system will protect the aircraft from both radar and infrared-guided threats. Currently, the MC-130E is equipped with aerial refueling pods to provide in-flight refueling of Special Operations Forces and combat search and rescue helicopters. The MC-130H will be modified to provide this capability in the near future.
The primary difference between the MC-130E and MC-130H involves the degree of integration of the mission computers and avionics suite. The Combat Talon I was conceived originally and developed during the 1960s, and although extensively upgraded in the 1980-90s it still features analog instrumentation and does not fully integrate the sensors and communications suites. The Combat Talon II, designed in the 1980s, features an integrated glass flight deck which improves crew coordination and reduces the crew complement by two.
General Characteristics
Primary Function: Infiltration, exfiltration and resupply of special operations forces
Builder: Lockheed
Power Plant: Four Allison T56-A-15 turboprop engines
Thrust: 4,910 shaft horsepower each engine
Length:
MC-130E: 100 feet, 10 inches (30.7 meters)
MC-130H: 99 feet, 9 inches (30.4 meters)
Height: 38 feet, 6 inches (11.7 meters)
Wingspan: 132 feet, 7 inches (40.4 meters)
Speed: 300 mph
Load:
MC-130E: 53 troops, 26 paratroopers
MC-130H: 77 troops, 52 paratroopers or 57 litter patients
Ceiling: 33,000 feet (10,000 meters)
Maximum Takeoff Weight:155,000 pounds (69,750 kilograms)
Range: 2,700 nautical miles (4,344 kilometers) Inflight refueling extends this to unlimited range
Crew:
MC-130E: Officers - two pilots, two navigators and an electronic warfare officer; enlisted - flight engineer, radio operator and two loadmasters
MC-130H: Officers - two pilots, a navigator and electronic warfare officer; enlisted - flight engineer and two loadmasters
Date Deployed: MC-130E, 1966; MC-130H, June 1991
Unit Cost: MC-130E, $75 million; MC-130H, $155 million (fiscal 2001 constant dollars)
Inventory: Active force, MC-130H, 24; Reserve, MC-130E, 14; ANG, 0
Point of Contact
U.S. Air Force Special Operations Command, Public Affairs Office; 229 Cody Ave, Ste 103; Hurlburt Field FL 32544-5312; DSN 579-5515 or (850) 884-5515
March 2003
|
|
Printable Fact Sheet
