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E-6B Mercury

E-6B Mercury

Communications Aircrafts
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Basic Information
Name
E-6B Mercury
Designation
E-6B Mercury
Alternate Designation
TACAMO (Take Charge and Move Out)
Equipment Type
Communications Aircrafts
Manufacturer
Boeing
Date of Introduction
1997
Description

The US Navy E-6 Mercury, also known as TACAMO (TAke Charge And Move Out), is a communications relay and an airborne command post aircraft derived from the Boeing 707 commercial aircraft. It provides survivable, reliable, and endurable command, control and communications between the National Command Authorities and strategic and non-strategic US forces worldwide. The E-6 aircraft replaced the aging EC-130Q performing airborne communications between the US national authorities and submarine ballistic forces during times of crisis. It carries a very low frequency communications dual trailing wire antennas. The first E-6A aircraft was accepted by the US Navy in 1989. The E-6B was conceived for the replacement of the EC-135 Looking Glass airborne command post aircraft, while retaining E-6A capabilities. The first aircraft entered service with the US Navy in 1997 and assumed its dual purpose operational mission in October 1998. The E-6B dual purpose aircraft (command post and communications link) was equipped with the Airborne Launch Control System (ALCS). ALCS is capable of launching land based intercontinental ballistic missiles. The E-6 fleet was completely upgraded to the B model standard in 2003 being powered by four CFM-56-2A-2 turbofans.

Air & Air Defense Specifications
Crew 22
Max Speed 961.2 km/h
Range 12150.0 km
Service Ceiling 12200 m
Wingspan 45.20 m
Overview (Deagel)
Group Communications Aircrafts
Status Active
Also Known As TACAMO (Take Charge and Move Out)
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) 1997
Total Production 16
Unitary Cost USD $142 million
Specifications (Deagel)
Crew 22
Number of Engines 4
Dimensions — Height 12.9 meter
Dimensions — Length 45.8 meter
Dimensions — Wingspan 45.2 meter
Mass — Max Takeoff Weight 154 ton
Performance — Ceiling 12,200 meter
Performance — Max Range 12,150 kilometer
Speed — Top Speed at High Altitude 267 mps
Time — Flight Endurance 6 hour
Gear (Deagel)
Item 1 Jamming Systems: AN/ALR-66B (1)
Item 2 Turbofan Engines: CFM56-2A (4)
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
45.8 m
Width
45.2 m
Height
12.9 m
Weight
154000 kg
Operators (1)
United States
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