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https://en.wikipedia.org/wiki/Aero_S...es_Super_Guppy
The Aero Spacelines Super Guppy is a large, wide-bodied cargo aircraft that is used for hauling outsize cargo components. It was the successor to the Pregnant Guppy, the first of the Guppy aircraft produced by Aero Spacelines. Five were built in two variants, both of which were colloquially referred to as the "Super Guppy". The Super Guppy is "the only airplane in the world capable of carrying a complete S-IVB stage", the third stage of the Saturn V rocket. The Super Guppy performed this role several times during the Apollo program. The first, the Super Guppy, or "SG", was built directly from the fuselage of a C-97J Turbo Stratocruiser, the military version of the 1950s Boeing 377 Stratocruiser passenger plane. The fuselage was lengthened to 141 feet (43 m), and ballooned out to a maximum inside diameter of 25 ft (7.6 m), the length of the cargo compartment being 94 ft 6 in (28.8 m). The floor of the cargo compartment was still only 8 ft 9 in (2.7 m) wide, as necessitated by the use of the Stratocruiser fuselage. In addition to the fuselage modifications, the Super Guppy used Pratt & Whitney T-34-P-7WA turboprop engines for increased power and range, and modified wing and tail surfaces. It could carry a load of 54,000 pounds (24,000 kg) and cruise at 300 mph (480 km/h). The second version was officially known as the Super Guppy Turbine (SGT), although it used turboprop engines like the first Super Guppy. This variant used Allison 501-D22C turboprops. Unlike the previous Guppy, the main portion of its fuselage was constructed from scratch. By building from scratch, Aero Spacelines was able to widen the floor of the cargo compartment to 13 ft (4.0 m). The overall cargo-compartment length was increased to 111 ft 6 in (34.0 m), and the improved fuselage and engines allowed for a maximum load of 52,500 lb (23,800 kg). These design improvements, combined with a pressurized crew cabin that allowed for higher-altitude cruising, allowed the SGT to transport more cargo than its predecessors. The SGT retained only the cockpit, wings, tail, and main landing gear of the 377. The nose gear was taken from a Boeing 707 and rotated 180 degrees. This dropped the front of the aircraft slightly, leveling the cargo-bay floor and simplifying loading operations. In the early 1970s, the two Super Guppy Turbines were used by Airbus to transport aeroplane parts from decentralised production facilities to the final assembly plant in Toulouse. In 1982 and 1983, two additional Super Guppy Turbines were built by Union de Transports Aériens Industries in France after Airbus bought the right to produce the aircraft. The four Super Guppies have since been replaced by the Airbus Beluga, capable of carrying twice as much cargo by weight. Variants Aero Spacelines B-377-SG Super Guppy, prototype of a much enlarged version of the Guppy using C-97J components, powered by four Pratt & Whitney T-34-P-7WA turbo-prop engines. Aero Spacelines B-377-SGT Super Guppy Turbine (Guppy 201), production version powered by Allison 501-D22C turbo-prop engines, using an enlarged cargo section built from scratch instead of being converted from original C-97J components. Role Outsize cargo aircraft Manufacturer Aero Spacelines / Airbus First flight August 31, 1965 Status Active, operated by NASA Primary users Aero Spacelines NASA, Airbus, Aeromaritime Number built 1 SG, 4 SGT Developed from C-97J Turbo Stratocruiser 377 Stratocruiser Pregnant Guppy (fourth SGT built with cannibalized pieces from PG) Specifications (Super Guppy Turbine) General characteristics Crew: Four Length: 143 ft 10 in (43.84 m) Wingspan: 156 ft 3 in (47.625 m) Height: 48 ft 6 in (14.78 m) Wing area: 1,964.6 ft2 (182.51 m2) Empty weight: 101,500 lb (46,039 kg) Useful load: 54,500 lb (24,720 kg) Max. takeoff weight: 170,000 lb (77,110 kg) Cargo bay dimensions: 111 ft × 25 ft × 25 ft (33.8 m × 7.62 m × 7.62 m) Powerplant: 4 × Allison 501-D22C turboprops, 4,680 hp (3,491 kW) each Performance Maximum speed: 250 knots (288 mph, 463 km/h) Cruise speed: 220 knots (253 mph, 407 km/h (economical cruise at 20,000 feet MSL)) Range: 1,734 nm (1,986 mi, 3,219 km) Service ceiling: 25,000 ft (certificated ceiling) (7620 m) Wing loading: 86.5 lb/ft2 (422.5 kg/m2) Power/mass: 9.08 lb/hp (5.52 kg/kW) * |
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