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Military


Airbus A300-600ST Beluga

A300-600 A300-600FA300-600F Beluga
Overall length 177 ft. 5 in. 177 ft. 5 in. 184 ft. 3 in.
Height 54 ft. 3 in. 54 ft. 3 in. 56 ft. 7 in.
Fuselage diameter 18 ft. 5 in. 18 ft. 6 in. 13 ft.
Maximum cabin width 17 ft. 4 in. 17 ft. 4 in. 12 ft. 2 in.
Cabin length 133 ft. 6 in. 133 ft. 6 in. 123 ft. 8 in.
Wingspan (geometric) 147 ft. 1 in. 147 ft. 1 in. 147 ft. 2 in.
Wing area (reference) 2,800 ft 2,800 ft2 1,317 ft2
Wing sweep (25% chord) 28 28 degrees 25 degrees
Wheelbase 61 ft. 1 in. 61 ft. 1 in. 36.25 ft.
Wheel track 31 ft. 6 in. 31 ft. 6 in. 25 ft.
BASIC OPERATING DATA
Engines two CF6-80C2 or PW4000 two CF6-80C2 or PW4000 GE CF6-80C2A8
Engine thrust range 56,000-61,500 lbs 56,000-61,500 lb. slst 26,752-26,977 lb. slst
Typical passenger seating 266 22 (23) 15 (21) pallets
Range (w/max. passengers) 1,950 (2,650) nm. 39.3-tons payload: 1,500 nm. / 25.6-tons payload: 2,500 nm.
Max. operating Mach number (Mmo)0.82 0.82 Mo. 0.82 Mo.
Bulk hold volume - Standard/option 361.0 398 ft3
DESIGN WEIGHTS
Maximum ramp weight 380.5 lbs. X 1000 377.9 (366) lbs. X 1000
Maximum takeoff weight 378.5 lbs. X 1000 375.9 (370.4) lbs. X 1000 341,713 lb.
Maximum landing weight 308.6 lbs. X 1000 308.6 (315.5) lbs. X 1000 308,644 lb.
Maximum zero fuel weight 286.6 lbs. X 1000 286.6 (300.9) lbs. X 1000 294,314 lb.
Maximum fuel capacity 18,000 US gal. 18,000 (11,730) US gal. 6,303 (8,520)(9,095) US gal.
Typical operating weight empty 200.4 lbs. X 1000 180.7 lbs. X 1000
Typical volumetric payload 76.9 lbs. X 1000 105.9 / 120.2 lbs. X 1000 103,616 lb.







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Page last modified: 11-07-2011 02:50:18 ZULU