#1
25th February 2016, 06:44 PM
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Boeing Indian Air Force
I want to get information about the Boeing Indian Air Force C-17 Globemaster III along with image. So here can you provide me information about it?
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#2
25th February 2016, 06:46 PM
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Re: Boeing Indian Air Force
If you want to get information about the Boeing Indian Air Force C-17 Globemaster III along with image, then here I am telling you about it, as you want. Boeing C-17 Globemaster III The prototype C-17, known as T-1, flying a test sortie in 2007. Role Strategic and tactical airlifter National origin United States Manufacturer McDonnell Douglas / Boeing First flight 15 September 1991 Introduction 17 January 1995 Status In service Primary users United States Air Force Royal Air Force Royal Australian Air Force Indian Air Force Produced 1991–2015 Number built 279 as of February 2015 Unit cost US$218 million (flyaway cost for FY2007) Developed from McDonnell Douglas YC-15 General characteristics Crew: 3: 2 pilots, 1 loadmaster (five additional personnel required for aeromedical evacuation) 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, three Strykers, or six M1117 Armored Security Vehicles Payload: 170,900 lb (77,519 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles Length: 174 ft (53 m) Wingspan: 169.8 ft (51.75 m) Height: 55.1 ft (16.8 m) Wing area: 3,800 ft² (353 m²) Empty weight: 282,500 lb (128,100 kg) Max. takeoff weight: 585,000 lb (265,350 kg) Powerplant: 4 × Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each Fuel capacity: 35,546 U.S. gal (134,556 L) Performance Cruise speed: Mach 0.74 (450 knots, 515 mph, 830 km/h) Range: 2,420 nmi[192] (2,785 mi, 4,482 km) ; 5,610 nmi (10,390 km) with paratroopers Service ceiling: 45,000 ft (13,716 m) Max. wing loading: 150 lb/ft² (750 kg/m²) Minimum thrust/weight: 0.277 Takeoff run at MTOW: 7,600 ft (2,316 m) Landing distance: 3,500 ft (1,060 m) Variants C-17A: Initial military airlifter version. C-17A "ER": Unofficial name for C-17As with extended range due to the addition of the center wing tank. This upgrade was incorporated in production beginning in 2001 with Block 13 aircraft. C-17B: Proposed tactical airlifter version. The design includes double-slotted flaps, an additional main landing gear on center fuselage, more powerful engines and other systems for shorter landing and take-off distances. Boeing offered the C-17B to the U.S. military in 2007 for carrying the Army's Future Combat Systems (FCS) vehicles and other equipment. MD-17: Proposed variant for civilian operators. Later re-designated as BC-17 after 1997 merger. Boeing Indian Air Force C-17 Globemaster III |