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Military Aircraft


Boeing E-6A Mercury

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The E-6A communications relay mission is accomplished by trailing dual wire antennas while performing a continuous orbit maneuver.  It is essential that the wires obtain as near a vertical attitude as possible for optimum very low frequency connectivity.  Currently, there exists orbit control problems and wire/tail contact causing bank-angle restrictions which precludes the E-6A from obtaining optimal wire verticality.  Modifications to the avionics systems are required to meet the orbit operational requirements.  The E-6A Orbit Improvement Program, which corrects theE-6A deficiency, consists of the installation of auto throttles and software improvements to the Flight Management Computer System (FMCS).
 

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Boeing Aircraft Length: 152 ft 11 in.
First Flight: February 19, 1987 Height: 42 ft. 5 in.
Model: A Wing Span: 148 ft. 4 in.
Crew: Four , up to five communications operators, or increased mission crew for extended or remote deployment assignments. Wing Area: 
Nickname: Mercury Empty Weight: 
Basic Role: long endurance communications relay. Max. Weight: 342,000 lb.
Other Versions:  E-6B Armament: None.
Principal User: USA.

Propulsion

Performance

Power Plant:  CFM-56-2A-2 High bypass turbofans.
Range: 7,307 miles. Horsepower: 24,000 lb.
Max. Speed: 610 mph. No. Of Engines: Four.
Ceiling: 42,000 ft.  
Climb Rate:   

 

 

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