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E-4B

E-4B

Communications Aircrafts
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Basic Information
Name
E-4B
Designation
E-4B
Alternate Designation
E-4A
Equipment Type
Communications Aircrafts
Manufacturer
Boeing
Date of Introduction
1980
Description

The US Air Force E-4 is an airborne operations center for the President and Secretary of Defense derived from Boeing 747-200 airliner. In case of national emergency or destruction of ground control centers, this aircraft provides a highly survivable command, control and communications center to direct US military forces. The E-4 can be refueled in-flight to extend its range and mission endurance. The E-4 was developed as the replacement for aging EC-135 command post aircraft while providing larger capacity due to its huge airframe. The E-4A was introduced in late 1974 and the B model was delivered to the US Air Force in January 1980. All four existing A models were converted to the B standard by 1985. Currently, it is powered by four 52,500-lb CF6-50E2 engines. The E-4B has electromagnetic pulse protection, nuclear and thermal effects shielding, an electrical system designed to support advanced electronics, and a wide variety of communications equipment. The communications system links to US strategic and tactical communication satellites constellations. At least one E-4B is always on alert at one of many selected bases throughout the world to support US national authorities in an emergency event. In December 2005 the US Air Force awarded an industry team led by Boeing a $2 billion contract as Product Support Integrator (PSI) for the E-4 National Airborne Operations Center fleet. The contract was for a five-year period plus one five-year option. The Boeing-led team included L3 Communications, Rockwell Collins, and Greenpoint Technology Inc.

Air & Air Defense Specifications
Crew 114
Service Ceiling 9100 m
Wingspan 59.70 m
Overview (Deagel)
Group Communications Aircrafts
Status Active
Also Known As E-4A
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) 1980
Total Production 4
Unitary Cost USD $223 million
Specifications (Deagel)
Crew 114
Number of Engines 4
Dimensions — Height 19.3 meter
Dimensions — Length 70.5 meter
Dimensions — Wingspan 59.7 meter
Mass — Max Takeoff Thrust 210,000 pound
Mass — Max Takeoff Weight 360 ton
Performance — Ceiling 9,100 meter
Time — Flight Endurance 12 hour
Gear (Deagel)
Item 1 Turbofan Engines: CF6-80C2 (4)
Item 2 Turbofan Engines: F103 (4)
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
70.5 m
Width
59.7 m
Height
19.3 m
Weight
360000 kg
Operators (1)
United States
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