Flat Wing Area
390.2857 m²
Cruise Speed
740.2982 km/h
Maximum Take-Off Weight
176.6742 t (paragliders: kg)
Maximum Range
4747.565 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Douglas C-132 |
176.6742 |
4747.565 |
Similar airplanes
All data (20 fields)
- Name
- Douglas C-132
- Manufacturer
- Douglas Aircraft Corporation
- Description
- The Douglas C-132 was an American military transport aircraft proposed in the 1950s by the Douglas Aircraft Company, based on the company's C-124 Globemaster II.
- Designer
- Douglas Aircraft Corporation
- Type
- Cargo transport
- Length (m)
- 55.7784
- Cockpit Crew
- 3
- Max Seating
- 800
- Cruise Speed (km/h)
- 740.2982
- Max Ceiling (m)
- 11887.2
- Capacity Description
- 800 troops
- National Origin
- United States of America
- Number Built
- 0
- Powerplant Description
- 4 × Pratt & Whitney T57-P-1 turboprop engines, 11185 kW (15000 hp) each
- Primary Users
- United States Air Force (intended)
- Status
- Cancelled in 1957
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Douglas_C-132
- Flat Wing Span (m)
- 56.6928
- Flat Wing Area (m²)
- 390.2857
- Number of Engines
- 4