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C-17 Globemaster III

The C-17 Globemaster III
Description
RoleCargo and Troop Transport
CrewThree (2 Pilots, 1 Loadmaster)
First Flight
Entered ServiceJune 1993
Manufacturer Boeing Integrated Defense Systems
Dimensions
Length174 ft. 0 in.53 m
Wingspan169 ft. 10 in.57.75 m
Height55 ft. 1 in.16.79 m
Wing Area3,800 ft.² (Main wing)
35.85 ft.² (Winglet)
353 m²
3.33 m²
Cargo Hold Dimensions88 ft. × 18 ft. × 12 ft. 4 in. 26.8 m × 5.5 m × 3.8 m
Weights
Empty lb. kg
Loaded lb. kg
Maximum Takeoff585,000 lb. (Current)
630,000 lb. (In testing)
265,500 kg
285,750 kg
Cargo170,900 lb.77,500 kg
Capacity102 troops/paratroops; 36 litter and 54 ambulatory patients with attendants
Powerplant
Engines4 × Pratt and Whitney F117-PW-100 turbofan engines
Thrust40,440 lbf180 kN
Performance
Maximum Speed450 kt. km/h
Combat Range2,400 n.m. (Base)
2,800 n.m. (ER)
4,444 km
5,186 km
Ferry Range6,250 n.m. 11,575 km
Service Ceiling45,000 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.

1 Mission

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.

2 Features

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.



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