E-6 Mercury
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| E-6 Mercury | |||
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| Missing image Mercury.e6b.300pix.jpg image:mercury.e6b.300pix.jpg E-6 Mercury. | |||
| Description | |||
| Role | |||
| Crew | 22 | ||
| Dimensions | |||
| Length | 45.8 m | ||
| Wingspan | 45.2 m | ||
| Height | 12.9 m | ||
| Wing area | |||
| Weights | |||
| Empty | |||
| Loaded | 154,400 kg | ||
| Maximum take-off | |||
| Powerplant | |||
| Engines | |||
| Power | Four CFMI CFM-56-2A-2 High bypass turbofans | ||
| Performance | |||
| Maximum speed | 960 km/h | ||
| Combat range | |||
| Ferry range | |||
| Service ceiling | 12,200 m | ||
| Rate of climb | |||
| Armament | |||
| Guns | |||
| Bombs | |||
The Boeing IDS E-6 Mercury is a United States of America military aircraft. It operates as an airborne command post and communications centre, relaying instructions from the National Command Authority. Its role in relaying to the fleet ballistic missile submarines gives it the suffix TACAMO ("Take Charge and Move Out").
The E-6 is found in two variants both built from a basic Boeing 707-320C. The E-6A was designed to replace the EC-130 and was accepted by the US Navy in August 1989, sixteen were delivered up to 1992. The E-6B was a modified E-6A with additional equipment and positions to replace the EC-135. The E-6B includes an airborne launch control system, allowing it to fire the US ICBM arsenal. The first E-6B was accepted in December 1997 and the entire E-6 fleet has now been modified to the E-6B standard.
E-6B
- Height: 12.9 m
- Weight: (Maximum) 154,400 kg
- Range: 12,144 km, with 6 hours loiter time
- Cost: $141.7 million
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