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E-2 Hawkeye vs E-7 Wedgetail

E-2 Hawkeye vs E-7 Wedgetail at a glance — top speed 648 vs 853 km/h, range 2,708 vs 6,500 km, max takeoff weight 57,500 vs 77,600 kg, built 313 vs 15 units.

Grumman E-2 Hawkeye military special mission aircraft side profile drawing
🇺🇸 E-2 Hawkeye
Boeing E-7 Wedgetail military special mission aircraft side profile drawing
🇺🇸 E-7 Wedgetail
Specifications
E-2 Hawkeye E-7 Wedgetail
Origin country 🇺🇸 United States 🇺🇸 United States
Category Military Special Mission Aircraft Military Special Mission Aircraft
Manufacturer Grumman Boeing
First flight 21 October 1960 1 January 2004
Year introduced 1964 2010
Number produced 313 units 15 units
Average unit price $232 million $400 million
Wing area 65.0 m² 91.0 m²
Wingspan 24.6 m 35.8 m
Height 5.6 m 12.5 m
Length 17.6 m 33.6 m
Maximum speed 648 km/h 853 km/h
Operational range 2,708 km 6,500 km
Service ceiling 10,577 m 12,500 m
Max. takeoff weight 57,500 kg 77,600 kg
Empty weight 19,536 kg 46,606 kg
Total thrust 2 x 3,803 kW 2 x 121 kN
Performance Radar Chart

Detailed Comparison

Northrop Grumman’s E-2 Hawkeye and Boeing’s E-7 Wedgetail execute the airborne early warning and control (AEW&C) mission through mutually exclusive airframe paradigms. The E-2 is a purpose-built, carrier-capable turboprop constrained by naval aviation geometries, while the E-7 leverages a commercial 737 Next Generation fuselage to mount a fixed electronically scanned array.

Development and Design

Grumman designed the E-2 in the late 1950s around the physical limitations of Essex-class carrier elevators. This dictated a high-wing, twin-turboprop configuration with a 24-foot rotating radome and a complex folding wing system. Subsequent iterations—culminating in the E-2D—retained the basic airframe while substituting mechanical radar components with the AN/APY-9 UHF radar. Conversely, Boeing developed the E-7 for the Royal Australian Air Force (RAAF) using a commercial 737-700ER airframe. The design abandons the rotating dome for a fixed Northrop Grumman Multi-role Electronically Scanned Array (MESA). The dorsal "top hat" achieves 360-degree coverage via side-looking and end-fire arrays, reducing aerodynamic drag compared to a rotodome while allowing dynamic radar sector allocation.

Specifications and Performances

The physical dimensions dictate vast differences in kinematics and crew capacity. The jet-powered E-7 operates at a maximum speed of 853 km/h and a service ceiling of 12,500 meters, outstripping the turboprop E-2’s 648 km/h and 10,577-meter ceiling. Altitude translates directly to radar horizon; the E-7's higher operating ceiling grants the MESA radar a look-up range exceeding 600 km. Endurance heavily favors the Boeing platform. The E-7 supports 17-hour missions with a 19-person mission crew managing up to ten consoles. The E-2 hits a 6-hour endurance limit unrefueled, compressing the workload onto three system operators in a cramped aft fuselage. The E-2’s $232 million unit cost sits far below the E-7’s $400 million price tag, reflecting the disparity in airframe volume and system scaling.

Deployment and usage

The US Navy integrated the E-2A in 1964. The platform generated combat data across Vietnam, the 1982 Lebanon War (operated by Israel), and Desert Storm. In 1981, a US Navy E-2 directed F-14s to down two Libyan Su-22s over the Gulf of Sidra. The E-7 is younger but actively displacing legacy E-3 fleets globally:

  • RAAF Wedgetails logged 17-hour command and control sorties over Iraq and monitor NATO's eastern flank.
  • Turkey operates four aircraft to patrol its southern airspace.
  • The Republic of Korea deploys the Peace Eye variant to monitor DPRK border activity.

The UK and USAF selected the E-7 to recapitalize their AWACS fleets, prioritizing the dispatch reliability of the commercial CFM56-7B27A engines.

Conclusion

The E-7 Wedgetail holds the absolute advantage in theater-level battle management. Its altitude edge, 6,500 km range, and commercial-derivative reliability allow it to manage dense air wars far longer than the Hawkeye. Land-based operators face no deck constraints and should procure the E-7. However, the E-2D Hawkeye retains a monopoly on blue-water carrier aviation. Navies operating CATOBAR carriers require the E-2’s specific aerodynamic compromises to project an organic AEW&C umbrella beyond the reach of land bases.

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Frequently Asked Questions

Which is faster, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail is faster with a maximum speed of 853 km/h compared to the E-2 Hawkeye's 648 km/h, a difference of 205 km/h.
Which has longer range, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail has a longer range at 6,500 km compared to the E-2 Hawkeye's 2,708 km.
Which can fly higher, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail has a higher service ceiling at 12,500 meters (41,010 ft) compared to the E-2 Hawkeye's 10,577 meters (34,701 ft).
Which is heavier, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail has a higher maximum takeoff weight at 77,600 kg compared to the E-2 Hawkeye's 57,500 kg.
Which is larger, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail is longer at 33.6 meters compared to the E-2 Hawkeye's 17.6 meters.
Which is more expensive, the E-2 Hawkeye or E-7 Wedgetail?
The E-7 Wedgetail is more expensive at approximately $400 million per unit compared to the E-2 Hawkeye at $232 million.
Which entered service first, the E-2 Hawkeye or E-7 Wedgetail?
The E-2 Hawkeye entered service first in 1964, 46 years before the E-7 Wedgetail which entered service in 2010.
Which has been built in greater numbers, the E-2 Hawkeye or E-7 Wedgetail?
The E-2 Hawkeye has been produced in greater numbers with 313 units compared to 15 units of the E-7 Wedgetail.