Monday, November 24, 2014

C-17 Globemaster III

C-17 Globemaster III (Strategic/Tactical airlifter) – 223


Manufacturer: McDonnell Douglas, Boeing
First flight: 15 September 1991
Introduction: 17 January 1995
Produced: 1991-present
Number built: 250 as of December 2012
Unit cost: $218 million (flyaway cost for FY2007)


Crew: 3: 2 pilots, 1 loadmaster
Length: 53 m
Wingspan: 51.75 m
Height: 16.8 m
Wing area: 353 m²
Empty weight: 128,100 kg
Max. takeoff weight: 265,350 kg
Powerplant: 4× Pratt & Whitney F117-PW-100 turbofans, 18,355 lbf (180 kN) each
Fuel capacity: 134,556 L


Cruise speed: Mach 0.74 (830 km/h)
Range: 4,482 km; 10,390 km with paratroopers
Service ceiling: 13,716 m
Max. wing loading: 750 kg/m²
Minimum thrust/weight: 0.277
Takeoff run at MTOW: 2,316 m
Landing distance: 1,060 m


Capacity:
102 paratroopers; or
134 troops with palletized and sidewall seats; or
54 troops with sidewall seats (allows 13 cargo pallets) only; or
36 litter and 54 ambulatory patients and medical attendants; or
Cargo, such as an M1 Abrams tank, 8 Strykers, or 6 M1117 Armored Security Vehicles


Payload: 77,519 kg of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles

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