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U. S. Military Aircraft

CH-47 Chinook

Photo by Salamander

The Western world's most important medium /heavy lift helicopter, the CH-47 is a lineal descendent of the twin rotor Piasecki helicopter of the late 1940s for piasecki became Vertol, which became Boeing CH-47 CHINOOK  Boeing  Vertol and finally Boeing Helicopters. Development of the Chinook began in 1956 and the first prototype flew in September 1961. The CH-47A, B, and C variants performed with great distinction in the Vietnam War, especially for tasks such as moving artillery. The Chinook is still a vital part of the US Army's inventory, and from 1976 large numbers of older CH-47s have been remanufactured as much improved CH-47Ds the first being redelivered in 1982 in a program to complete 436 machine by 1993. 

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Boeing Height: 18 ft. 7.75 in.
First Flight: September 1961 Empty Weight:   23,903 lb. 
Model: D Max. Weight: 54,000 lb. 
Crew: Two /Three Pay Load: 28,000 lb.
Nickname: Chinook

Dimensions

Basic Role: Medium lift helicopter.  Main Rotor Diameter: 60 ft. 0 in 
Other Versions: CH-47A: with 2,200-shp/1,641-kW T55-L-5 turbo shafts, CH-47B: with 2,850-shp/2,125-kW T55-L-7Cs, CH-47C: with 3,750-shp/2,796-kW T55-L-11As, strengthened transmission, and greater fuel capacity, CH-47D: re-manufactured type with 13 major improvements, international Chinook (main export variant, MH-47E: an armored and armed version for the US Special Forces, CH-147: Ch-47C for Canada, and Chinook HC.Mk 1 British helicopters to CH-147 standard but with greater power. Length Overall Rotor Turning: 9 ft.0 in. 
Principal User : Argentina, Australia, Canada, Great Britain, Japan, Spain, Thailand, and USA. Main Rotor Disk Area: 5,655.0 sq. ft. 

Performance

Propulsion

Range: Radius 115 miles.  Power Plant: Lycoming T55-L-712 turbo shafts.  
Max. Speed: 188 mph.  Horsepower: 4,500-shp. 
Ceiling: 22,100 ft.  No. Of Engines: Two  
Climb Rate: 1,490 ft. per minute.   

 

 

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