C-97 Stratofreighter

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(Redirected from C-97 Stratocruiser)
Boeing C-97 Stratofreighter
Image:Boeing C97.jpg
Description
RoleMilitary Transport
Crew4
Capacity3,000 ft³85 m³
First FlightNovember 15, 1944
Entered Service
ManufacturerBoeing
Dimensions
Length110ft 4in33.7 m
Wingspan141ft 3in43.1 m
Height38ft 3in11.7 m
Wing Area1,734 ft²161.1 m²
Weights
Empty82,500 lb37,410 kg
Loaded120,000 lb54,420 kg
Maximum takeoff175,000 lb79,370 kg
Powerplant
Engine4 × Pratt & Whitney Wasp Major
Power (each)3,500 hp2,610 kW
Performance
Maximum speed375 mph603 km/h
Combat range4,300 miles6,920 km
Ferry range km miles
Service ceiling35,000 ft10,670 m
Rate of climb ft/min m/min
Wing loading69.2 lb/ft²337.8 kg/m²
Power/Mass0.117 hp/lb0.192 kW/kg
Armament
none

The Boeing C-97 Stratofreighter was developed towards the end of World War II by fitting an enlarged upper fuselage onto a lower fuselage and wings which were essentially the same as the B-29 Superfortress. The prototype XC-97 was powered by the 2,200 hp (1,640 kW) Wright R-3350 engine, and even with this the performance was impressive — on January 11. 1945 the first prototype flew from Seattle to Washington, DC in 6 hours 4 minutes, an average speed of 383 mph (616 km/h). For the remaining models the powerplants were upgraded to the 3500 hp (2,610 kW) Pratt & Whitney Wasp Major.

The military transport had a useful payload of 35,000 lb (16 t) and could carry two normal trucks or light tanks. Loading was by a retractable ramp into doors in the bottom of the fuselage, which was pressurised in flight.

About 60 C-97 transports were built, but the design really flourished in the guise of the KC-97 Stratotanker flight-refuelling tanker. The civilian derivative Boeing 377 Stratocruiser was highly influential in the post-war development of long-distance civil aviation.

Operators

  • Israel, Spain, United States,

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