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| Contents | ||
| C-17 Globemaster III | ||
|---|---|---|
The C-17 Globemaster III | ||
| Description | ||
| Role | Cargo and Troop Transport | |
| Crew | Three (2 Pilots, 1 Loadmaster) | |
| First Flight | ||
| Entered Service | June 1993 | |
| Manufacturer | Boeing Integrated Defense Systems | |
| Dimensions | ||
| Length | 174 ft. 0 in. | 53 m |
| Wingspan | 169 ft. 10 in. | 57.75 m |
| Height | 55 ft. 1 in. | 16.79 m |
| Wing Area | 3,800 ft.² (Main wing) 35.85 ft.² (Winglet) | 353 m² 3.33 m² |
| Cargo Hold Dimensions | 88 ft. × 18 ft. × 12 ft. 4 in. | 26.8 m × 5.5 m × 3.8 m |
| Weights | ||
| Empty | lb. | kg |
| Loaded | lb. | kg |
| Maximum Takeoff | 585,000 lb. (Current) 630,000 lb. (In testing) | 265,500 kg 285,750 kg |
| Cargo | 170,900 lb. | 77,500 kg |
| Capacity | 102 troops/paratroops; 36 litter and 54 ambulatory patients with attendants | |
| Powerplant | ||
| Engines | 4 × Pratt and Whitney F117-PW-100 turbofan engines | |
| Thrust | 40,440 lbf | 180 kN |
| Performance | ||
| Maximum Speed | 450 kt. | km/h |
| Combat Range | 2,400 n.m. (Base) 2,800 n.m. (ER) | 4,444 km 5,186 km |
| Ferry Range | 6,250 n.m. | 11,575 km |
| Service Ceiling | 45,000 ft. | 13,710 m |
| Rate of Climb | ft./min | m/min |
| Wing Loading | lb./ft.² | kg/m² |
| Thrust/Weight | ||
| Power/Mass | hp/lb. | kW/kg |
| Avionics | ||
| Avionics | ||
| Armament | ||
| Guns | ||
| Bombs | ||
| Missiles | ||
| Rockets | ||
| Other | ||
The C-17 Globemaster III is a strategic airlifter manufactured by Boeing IDS, used by the United States Air Force and the Royal Air Force.
The C-17 Globemaster III is the newest, most flexible cargo aircraft to enter the airlift force. The C-17 is capable of rapid strategic delivery of troops and all types of cargo to main operating bases or directly to forward bases in the deployment area. The aircraft is also capable of performing tactical airlift and airdrop missions when required. The inherent flexibility and performance of the C-17 force improve the ability of the total airlift system to fulfill the worldwide air mobility requirements of the United States.
The ultimate measure of airlift effectiveness is the ability to rapidly project and sustain an effective combat force close to a potential battle area. Threats to U.S. interests have changed in recent years, and the size and weight of U.S. mechanized firepower and equipment have grown in response to improved capabilities of potential adversaries. This trend has significantly increased air mobility requirements, particularly in the area of large or heavy outsize cargo. As a result, newer and more flexible airlift aircraft are needed to meet potential armed contingencies, peacekeeping or humanitarian missions worldwide. The C-17 is capable of meeting today's demanding airlift missions.
Reliability and maintainability are two outstanding benefits of the C-17 system. Current operational requirements impose demanding reliability and maintainability. These requirements include an aircraft mission completion success probability rate of 92 percent, only 20 aircraft maintenance man-hours per flying hour, and full and partial mission availability rates of 74.7 and 82.5 percent, respectively. The Boeing warranty assures these figures will be met.
The C-17 measures 174 ft. long (53 m) with a wingspan of 169 ft. 10 in. (51.75 m). The aircraft is powered by four, fully reversible, Federal Aviation Administration–certified F117-PW-100 turbofan engines (the military designation for the commercial Pratt and Whitney PW2040), currently used on the Boeing 757. Each engine is rated at 40,440 lbf (180 kN) of thrust. The thrust reversers direct the flow of air upward and forward to avoid ingestion of dust and debris. Maximum use has been made of off-the-shelf and commercial equipment, including Air Force–standardized avionics.
The aircraft is operated by a crew of three (pilot, copilot, and loadmaster), reducing manpower requirements, risk exposure and long-term operating costs. Cargo is loaded onto the C-17 through a large aft door that accommodates military vehicles and palletized cargo. The C-17 can carry virtually all of the Army's air-transportable equipment.
Maximum payload capacity of the C-17 is 170,900 lb. (77,519 kg), and its maximum gross takeoff weight is 585,000 lb. (265,352 kg). With a payload of 160,000 lb. (72,575 kg) and an initial cruise altitude of 28,000 ft. (8,534 m), the C-17 has an unrefueled range of approximately 2,400 n.m. (4,445 km) on the first 71 units, and 2,800 n.m. (5,186 km) on all subsequent units, which are extended-range models with an additional fuel tank in the center wing box. Its cruise speed is approximately 450 kt. (833 km/h) (.74 Mach). The C-17 is designed to airdrop 102 paratroopers and equipment.
The design of the aircraft allows it to operate through small, austere airfields. The C-17 can take off and land on runways as short as 3,000 ft. (914 m) and only 90 ft. wide (27.4 m). Even on such narrow runways, the C-17 can turn around using a three-point star turn and its backing capability.