Flat Wing Area
233.1866 m²
Cruise Speed
341.1809 km/h
Maximum Take-Off Weight
78.0179 t (paragliders: kg)
Total Fuel Capacity
41639.53
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Douglas C-74 Globemaster |
78.0179 |
41639.53 |
5471.77 |
Similar airplanes
All data (25 fields)
- Name
- Douglas C-74 Globemaster
- Manufacturer
- Douglas Aircraft Corporation
- Description
- The Douglas C-74 Globemaster was a United States heavy-lift cargo aircraft built by the Douglas Aircraft Company in Long Beach, California.
- First Flight
- 1945-09-05
- Production End
- 1947-01-01
- Service End
- 1969-01-01
- Designer
- Douglas Aircraft Corporation
- Type
- Strategic airlifter
- Length (m)
- 37.7952
- Height (m)
- 13.1064
- Cockpit Crew
- 13
- Max Seating
- 125
- Max Speed (km/h)
- 527.8648
- Cruise Speed (km/h)
- 341.1809
- Max Ceiling (m)
- 6492.24
- Rate of Climb (m/s)
- 13.2334
- Capacity Description
- 125 troops, 115 stretchers with medical staff, or up to 48150 lb of cargo
- Number Built
- 14
- Powerplant Description
- 4 × Pratt & Whitney R-4360-69 Wasp Major /-29s /-49s 28-cylinder air-cooled 4-row radial piston engines, 2424 kW (3250 hp) each
- Primary Users
- United States Army Air Forces, United States Air Force
- Status
- Retired – 1959 (military), 1969 (civilian)
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Douglas_C-74_Globemaster
- Flat Wing Span (m)
- 52.7304
- Flat Wing Area (m²)
- 233.1866
- Number of Engines
- 4