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U. S. Military Aircraft

Boeing EC-135

 Photo by Coil B. Thouanel

At the beginning of the 1960s, Strategic Air Command decided to add to its inventory a number of flying command post which might survive any nuclear exchange that might knock out ground headquarters. Thus 17 KC-135B tankers, power by 18,000-lb thrust Pratt & Whitney TF33-P-5 turbofans, were reconfigured as EC-135C flying command post with a command space, rest area, and extensive communication facilities. The success of the EC-135C prompted a number of complementary conversions of the basis of the turbojet-power KC-135A. First came six EC-135A communication relay aircraft able to double in the command post role. other models followed, and some 40 or more aircraft remain in service for command and associated tasks.

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Boeing Length: 136 ft. 3 in. 
Date Deployed: August 1965 Height: 41 ft. 8 in. 
Model: A Wing Span: 130 ft. 10 in. 
Crew: Four Wing Area: 2,433.0 sq. ft. 
Nickname:  Empty Weight: 98,466 lb. 
Basic Role: Aerial command post and communication relay plane.  Max. Weight: 297,000 lb. 
Other Versions: EC-135A: Communication relay, EC-135C: SAC post attack command control system aircraft, EC-135G: ICBM launch control center aircraft, EC-135H: command post, EC-135J: upgraded EC-135Cs, EC-135K: Tactical Air Command post, EC-135L: relay aircraft, EC-135P: Pacific Air Forces command post. Armament: None 
Principal User: U. S. A.   

Performance

Propulsion

Range: 1,500 miles with 150,000 pounds of transfer fuel ferry mission, up to 11,015 miles.  Power Plant: Pratt & Whitney J57-P-59W turbojet.  
Max. Speed: 585 mph. Horsepower: 13,750-lb thrust. 
Ceiling: 50,000 ft. No. Of Engines: Four  
Climb Rate: 2,000 ft. per minute.   

 

 

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