Douglas C-133 Cargomaster

Airplanes

Length

47.01 m

Flat Wing Span

54.78 m

Height

14.7 m

Flat Wing Area

248.3298 m²

Max Seating

200

Cruise Speed

520.4116 km/h

Max Speed

577.8235 km/h

Max Ceiling

9128.76 m

Number of Engines

First Flight

1956-04-23

Number Built

Maximum Take-Off Weight

129.7274 t (paragliders: kg)

Maximum Range

6593.12 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Douglas C-133 Cargomaster	129.7274	6593.12

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Myasishchev VM-T		51.23	53.14		Compare
Beriev A-100		46.59	50.5		Compare
Tupolev Tu-95LAL		46.2	50.1		Compare
Vickers VC10	Rolls-Royce Conway	48.1584	44.5008	151	Compare
Lockheed C-141 Starlifter	Pratt & Whitney JT3D	51.3	48.8		Compare
Boeing CC-137	Pratt & Whitney JT3D	46.61	44.42	170	Compare

All data (26 fields)

Name: Douglas C-133 Cargomaster
Manufacturer: Douglas Aircraft Corporation
Description: The Douglas C-133 Cargomaster is an American large turboprop cargo aircraft built between 1956 and 1961 by the Douglas Aircraft Company for use with the United States Air Force.
ICAO Code: C133
First Flight: 1956-04-23
Production End: 1961-01-01
Service End: 1971-01-01
Designer: Douglas Aircraft Corporation
Type: Military transport aircraft
Length (m): 47.01
Height (m): 14.7
Max Seating: 200
Max Speed (km/h): 577.8235
Cruise Speed (km/h): 520.4116
Max Ceiling (m): 9128.76
Rate of Climb (m/s): 6.5024
Capacity Description: 200 passengers or 110000 lb
National Origin: United States of America
Number Built: 50
Powerplant Description: 4 × Pratt & Whitney T34-P-9W turboprop engines, 5593 kW (7500 hp) each
Primary Users: United States Air Force, NASA
Wikipedia Article (URL): en.wikipedia.org/wiki/Douglas_C-133_Cargomaster
Flat Wing Span (m): 54.78
Flat Wing Area (m²): 248.3298
Wake Category: M
Number of Engines: 4