MC-130
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| MC-130 Combat Talon | ||
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| Missing image MC-130EH.jpg | ||
| Description | ||
| Role | Infiltration, exfiltration and resupply of special operations forces | |
| Crew: | ||
| MC-130E: 9 | ||
| MC-130H: 7 | ||
| Entered Service: | ||
| MC-130E: 1966 | ||
| MC-130H: 1991 | ||
| Manufacturer | Lockheed | |
| Dimensions | ||
| Length | ||
| MC-130E | 100 feet, 10 inches | 30.7 meters |
| MC-130H | 99 feet, 9 inches | 30.4 meters |
| Wingspan | 132 ft, 7 in | 40.4 m |
| Height | 38 ft 6 in | 11.7 m |
| Wing area | ft² | m² |
| Weights | ||
| Empty | lb | kg |
| Loaded | lb | kg |
| Maximum takeoff | 155,000 lb | 69,750 kg |
| Capacity: | ||
| MC-130E | 53 troops, 26 paratroopers | |
| MC-130H | 77 troops, 52 paratroopers or 57 litter patients | |
| Powerplant | ||
| Engines | Four Allison T56-A-15 turboprop enginess | |
| Power | 4,910 hp each | 3,660 kW each |
| Performance | ||
| Maximum speed | 300 mph | 480 km/h |
| Combat Range | miles | 4,344 kilometers |
| Ferry Range | miles | km |
| Service ceiling | 33,000 ft | 10,000m |
| Rate of climb | ft/min | m/min |
| Wing loading | lb/ft² | kg/m² |
| Thrust/Weight | ||
| Power/Mass | hp/lb | kW/kg |
| Avionics | ||
| Avionics | Terrain-following and terrain-avoidance radars, ECM | |
| Armament | ||
| None | ||
The MC-130E/H COMBAT TALON I/II is a special operations variant of the C-130 aircraft operated by the USAF.
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.
Source
This article contains information that originally came from a US Government website, in the public domain. [USAF Website (http://www.af.mil/factsheets/factsheet.asp?fsID=115)]
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