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Boeing E-3 Sentry

The Boeing E-3 Sentry is an American airborne early warning and control (AEW&C) aircraft developed by Boeing. E-3s are commonly known as AWACS (Airborne Warning and Control System).

Derived from the Boeing 707 airliner, it provides all-weather surveillance, command, control, and communications, and is used by the United States Air Force, NATO, French Air and Space Force, and Royal Saudi Air Force.

The E-3 is distinguished by the distinctive rotating radar dome (rotodome) above the fuselage.

Production ended in 1992 after 68 aircraft had been built.

Variants

EC-137D-2

Prototype AWACS aircraft with JT3D engines, 1 fitted with a Westinghouse Electric radar and 1 with a Hughes Aircraft Company radar.

Both converted to E-3A standard with TF33 engines.

E-3A

Production aircraft with TF33 engines and AN/APY-1 radar, 24 built for USAF (later converted to E-3B standard), total of 34 ordered, the last 9 were completed as E-3Cs.

One additional aircraft retained by Boeing for testing, 18 built for NATO with TF33 engines and 5 for Saudi Arabia with CFM56 engines.

KE-3A

These are not AWACS aircraft but CFM56 powered tankers based on the E-3 design.

8 were sold to Saudi Arabia.

E-3B

E-3As with improvements.

E-3C

Production aircraft with AN/APY-2 radar, additional electronic consoles and system improvements.

JE-3C

One E-3A aircraft used by Boeing for trials later redesignated E-3C.

E-3D

Production aircraft for the RAF to E-3C standard with CFM56 engines and British modifications designated Sentry AEW.1.

Modifications included the addition of a refuelling probe next to the existing boom AAR receptacle, CFM-56 engines, wingtip ESM pods, an enhanced Maritime Surveillance Capability (MSC) offering Maritime Scan-Scan Processing (MSSP), JTIDS and Havequick 2 radios.

E-3F

Production aircraft for the French Air and Space Force to E-3C standard with CFM56 engines and French modifications.

E-3G

USAF Block 40/45 modification.

Includes hardware and software upgrades to improve communications, computer processing power, threat tracking, and others, and automates some previously manual functions.

Specifications

Crew

4

Mission crew

13–19

Length

152 ft 11 in (46.61 m)

Wingspan

145 ft 9 in (44.42 m)

Height

41 ft 4 in (12.60 m)

Wing area

3,050 sq ft (283 m2)

Empty weight

185,000 lb (83,915 kg)

Gross weight

344,000 lb (156,036 kg)

Max take-off weight

347,000 lb (157,397 kg)

Powerplant

4 × Pratt and Whitney TF33-PW-100A turbofan,

21,500 lbf (96 kN) thrust each

Performance

Maximum speed

461 kn (531 mph, 854 km/h)

Cruise speed

310 kn (360 mph, 580 km/h) optimum

Range

4,000 nmi (4,600 mi, 7,400 km)

Endurance

More than 8 hours without refuelling

Service ceiling

29,000 ft (8,800 m) minimum

Avionics

AN/APS-133 colour weather radar

Westinghouse Corporation AN/APY-1

Or

AN/APY-2 passive electronically scanned array radar system.

 

 

 

 

 

 

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